CONTROLLING LIU SYSTEM WITH DIFFERENT METHODS

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Robust Control

Robust Control

Robust ControlRobust control is a branch of control theory that deals with the design of controllers that are able to handle uncertainties and disturbances in the system. The main objective of robust control is to ensure that the system remains stable and performs as expected even in the presence of uncertainties and disturbances. In this essay, I will discuss the importance of robust control, the challenges associated with its implementation, and some of the techniques used to design robust controllers.Robust control is important because most real-world systems are subject to uncertainties and disturbances. For example, in a chemical process, the temperature, pressure, and flow rate may vary due to changes in the environment or equipment failure. Similarly, in a robotic system, the position, velocity, and acceleration of the robot may be affected by external forces such as wind or friction. Robust control ensures that the system remains stable and performs as expected even in the presence of these uncertainties and disturbances.However, implementing robust control is not easy. One of the main challengesis modeling the uncertainties and disturbances accurately. In many cases, the exact nature and magnitude of the uncertainties and disturbances are not known, and therefore, it is difficult to model them accurately. This can lead to overdesign or underdesign of the controller, which can result in poor performance or instability of the system.Another challenge is the trade-off between robustness and performance. A controller that is designed to be robust may not necessarily perform well in terms of tracking accuracy or disturbance rejection. On the other hand, a controllerthat is designed for optimal performance may not be robust enough to handle uncertainties and disturbances. Therefore, it is important to strike a balance between robustness and performance when designing a controller.To overcome these challenges, various techniques have been developed for designing robust controllers. One such technique is H-infinity control, which is a popular method for designing robust controllers. H-infinity control aims to minimize the effect of uncertainties and disturbances on the system by optimizing a performance criterion that takes into account the worst-case scenario. Thisensures that the system remains stable and performs as expected even in the presence of uncertainties and disturbances.Another technique is mu-synthesis, which is a method for designing controllers that are robust to model uncertainties. Mu-synthesis involves optimizing the controller design by taking into account the worst-case scenario of model uncertainties. This ensures that the controller is able to handle uncertainties in the system and maintain stability and performance.In conclusion, robust control is an important aspect of control theory that deals with the design of controllers that are able to handle uncertainties and disturbances in the system. However, implementing robust control is not easy due to the challenges associated with modeling uncertainties and disturbances accurately and balancing robustness and performance. To overcome these challenges, various techniques have been developed for designing robust controllers, such as H-infinity control and mu-synthesis. These techniques ensure that the system remains stable and performs as expected even in the presence of uncertainties and disturbances.。

Native Instruments MASCHINE MK3 用户手册说明书

Native Instruments MASCHINE MK3 用户手册说明书

The information in this document is subject to change without notice and does not represent a commitment on the part of Native Instruments GmbH. The software described by this docu-ment is subject to a License Agreement and may not be copied to other media. No part of this publication may be copied, reproduced or otherwise transmitted or recorded, for any purpose, without prior written permission by Native Instruments GmbH, hereinafter referred to as Native Instruments.“Native Instruments”, “NI” and associated logos are (registered) trademarks of Native Instru-ments GmbH.ASIO, VST, HALion and Cubase are registered trademarks of Steinberg Media Technologies GmbH.All other product and company names are trademarks™ or registered® trademarks of their re-spective holders. Use of them does not imply any affiliation with or endorsement by them.Document authored by: David Gover and Nico Sidi.Software version: 2.8 (02/2019)Hardware version: MASCHINE MK3Special thanks to the Beta Test Team, who were invaluable not just in tracking down bugs, but in making this a better product.NATIVE INSTRUMENTS GmbH Schlesische Str. 29-30D-10997 Berlin Germanywww.native-instruments.de NATIVE INSTRUMENTS North America, Inc. 6725 Sunset Boulevard5th FloorLos Angeles, CA 90028USANATIVE INSTRUMENTS K.K.YO Building 3FJingumae 6-7-15, Shibuya-ku, Tokyo 150-0001Japanwww.native-instruments.co.jp NATIVE INSTRUMENTS UK Limited 18 Phipp StreetLondon EC2A 4NUUKNATIVE INSTRUMENTS FRANCE SARL 113 Rue Saint-Maur75011 ParisFrance SHENZHEN NATIVE INSTRUMENTS COMPANY Limited 5F, Shenzhen Zimao Center111 Taizi Road, Nanshan District, Shenzhen, GuangdongChina© NATIVE INSTRUMENTS GmbH, 2019. All rights reserved.Table of Contents1Welcome to MASCHINE (25)1.1MASCHINE Documentation (26)1.2Document Conventions (27)1.3New Features in MASCHINE 2.8 (29)1.4New Features in MASCHINE 2.7.10 (31)1.5New Features in MASCHINE 2.7.8 (31)1.6New Features in MASCHINE 2.7.7 (32)1.7New Features in MASCHINE 2.7.4 (33)1.8New Features in MASCHINE 2.7.3 (36)2Quick Reference (38)2.1Using Your Controller (38)2.1.1Controller Modes and Mode Pinning (38)2.1.2Controlling the Software Views from Your Controller (40)2.2MASCHINE Project Overview (43)2.2.1Sound Content (44)2.2.2Arrangement (45)2.3MASCHINE Hardware Overview (48)2.3.1MASCHINE Hardware Overview (48)2.3.1.1Control Section (50)2.3.1.2Edit Section (53)2.3.1.3Performance Section (54)2.3.1.4Group Section (56)2.3.1.5Transport Section (56)2.3.1.6Pad Section (58)2.3.1.7Rear Panel (63)2.4MASCHINE Software Overview (65)2.4.1Header (66)2.4.2Browser (68)2.4.3Arranger (70)2.4.4Control Area (73)2.4.5Pattern Editor (74)3Basic Concepts (76)3.1Important Names and Concepts (76)3.2Adjusting the MASCHINE User Interface (79)3.2.1Adjusting the Size of the Interface (79)3.2.2Switching between Ideas View and Song View (80)3.2.3Showing/Hiding the Browser (81)3.2.4Showing/Hiding the Control Lane (81)3.3Common Operations (82)3.3.1Using the 4-Directional Push Encoder (82)3.3.2Pinning a Mode on the Controller (83)3.3.3Adjusting Volume, Swing, and Tempo (84)3.3.4Undo/Redo (87)3.3.5List Overlay for Selectors (89)3.3.6Zoom and Scroll Overlays (90)3.3.7Focusing on a Group or a Sound (91)3.3.8Switching Between the Master, Group, and Sound Level (96)3.3.9Navigating Channel Properties, Plug-ins, and Parameter Pages in the Control Area.973.3.9.1Extended Navigate Mode on Your Controller (102)3.3.10Navigating the Software Using the Controller (105)3.3.11Using Two or More Hardware Controllers (106)3.3.12Touch Auto-Write Option (108)3.4Native Kontrol Standard (110)3.5Stand-Alone and Plug-in Mode (111)3.5.1Differences between Stand-Alone and Plug-in Mode (112)3.5.2Switching Instances (113)3.5.3Controlling Various Instances with Different Controllers (114)3.6Host Integration (114)3.6.1Setting up Host Integration (115)3.6.1.1Setting up Ableton Live (macOS) (115)3.6.1.2Setting up Ableton Live (Windows) (116)3.6.1.3Setting up Apple Logic Pro X (116)3.6.2Integration with Ableton Live (117)3.6.3Integration with Apple Logic Pro X (119)3.7Preferences (120)3.7.1Preferences – General Page (121)3.7.2Preferences – Audio Page (126)3.7.3Preferences – MIDI Page (130)3.7.4Preferences – Default Page (133)3.7.5Preferences – Library Page (137)3.7.6Preferences – Plug-ins Page (145)3.7.7Preferences – Hardware Page (150)3.7.8Preferences – Colors Page (154)3.8Integrating MASCHINE into a MIDI Setup (156)3.8.1Connecting External MIDI Equipment (156)3.8.2Sync to External MIDI Clock (157)3.8.3Send MIDI Clock (158)3.9Syncing MASCHINE using Ableton Link (159)3.9.1Connecting to a Network (159)3.9.2Joining and Leaving a Link Session (159)3.10Using a Pedal with the MASCHINE Controller (160)3.11File Management on the MASCHINE Controller (161)4Browser (163)4.1Browser Basics (163)4.1.1The MASCHINE Library (163)4.1.2Browsing the Library vs. Browsing Your Hard Disks (164)4.2Searching and Loading Files from the Library (165)4.2.1Overview of the Library Pane (165)4.2.2Selecting or Loading a Product and Selecting a Bank from the Browser (170)4.2.2.1[MK3] Browsing by Product Category Using the Controller (174)4.2.2.2[MK3] Browsing by Product Vendor Using the Controller (174)4.2.3Selecting a Product Category, a Product, a Bank, and a Sub-Bank (175)4.2.3.1Selecting a Product Category, a Product, a Bank, and a Sub-Bank on theController (179)4.2.4Selecting a File Type (180)4.2.5Choosing Between Factory and User Content (181)4.2.6Selecting Type and Character Tags (182)4.2.7List and Tag Overlays in the Browser (186)4.2.8Performing a Text Search (188)4.2.9Loading a File from the Result List (188)4.3Additional Browsing Tools (193)4.3.1Loading the Selected Files Automatically (193)4.3.2Auditioning Instrument Presets (195)4.3.3Auditioning Samples (196)4.3.4Loading Groups with Patterns (197)4.3.5Loading Groups with Routing (198)4.3.6Displaying File Information (198)4.4Using Favorites in the Browser (199)4.5Editing the Files’ Tags and Properties (203)4.5.1Attribute Editor Basics (203)4.5.2The Bank Page (205)4.5.3The Types and Characters Pages (205)4.5.4The Properties Page (208)4.6Loading and Importing Files from Your File System (209)4.6.1Overview of the FILES Pane (209)4.6.2Using Favorites (211)4.6.3Using the Location Bar (212)4.6.4Navigating to Recent Locations (213)4.6.5Using the Result List (214)4.6.6Importing Files to the MASCHINE Library (217)4.7Locating Missing Samples (219)4.8Using Quick Browse (221)5Managing Sounds, Groups, and Your Project (225)5.1Overview of the Sounds, Groups, and Master (225)5.1.1The Sound, Group, and Master Channels (226)5.1.2Similarities and Differences in Handling Sounds and Groups (227)5.1.3Selecting Multiple Sounds or Groups (228)5.2Managing Sounds (233)5.2.1Loading Sounds (235)5.2.2Pre-listening to Sounds (236)5.2.3Renaming Sound Slots (237)5.2.4Changing the Sound’s Color (237)5.2.5Saving Sounds (239)5.2.6Copying and Pasting Sounds (241)5.2.7Moving Sounds (244)5.2.8Resetting Sound Slots (245)5.3Managing Groups (247)5.3.1Creating Groups (248)5.3.2Loading Groups (249)5.3.3Renaming Groups (251)5.3.4Changing the Group’s Color (251)5.3.5Saving Groups (253)5.3.6Copying and Pasting Groups (255)5.3.7Reordering Groups (258)5.3.8Deleting Groups (259)5.4Exporting MASCHINE Objects and Audio (260)5.4.1Saving a Group with its Samples (261)5.4.2Saving a Project with its Samples (262)5.4.3Exporting Audio (264)5.5Importing Third-Party File Formats (270)5.5.1Loading REX Files into Sound Slots (270)5.5.2Importing MPC Programs to Groups (271)6Playing on the Controller (275)6.1Adjusting the Pads (275)6.1.1The Pad View in the Software (275)6.1.2Choosing a Pad Input Mode (277)6.1.3Adjusting the Base Key (280)6.1.4Using Choke Groups (282)6.1.5Using Link Groups (284)6.2Adjusting the Key, Choke, and Link Parameters for Multiple Sounds (286)6.3Playing Tools (287)6.3.1Mute and Solo (288)6.3.2Choke All Notes (292)6.3.3Groove (293)6.3.4Level, Tempo, Tune, and Groove Shortcuts on Your Controller (295)6.3.5Tap Tempo (299)6.4Performance Features (300)6.4.1Overview of the Perform Features (300)6.4.2Selecting a Scale and Creating Chords (303)6.4.3Scale and Chord Parameters (303)6.4.4Creating Arpeggios and Repeated Notes (316)6.4.5Swing on Note Repeat / Arp Output (321)6.5Using Lock Snapshots (322)6.5.1Creating a Lock Snapshot (322)6.5.2Using Extended Lock (323)6.5.3Updating a Lock Snapshot (323)6.5.4Recalling a Lock Snapshot (324)6.5.5Morphing Between Lock Snapshots (324)6.5.6Deleting a Lock Snapshot (325)6.5.7Triggering Lock Snapshots via MIDI (326)6.6Using the Smart Strip (327)6.6.1Pitch Mode (328)6.6.2Modulation Mode (328)6.6.3Perform Mode (328)6.6.4Notes Mode (329)7Working with Plug-ins (330)7.1Plug-in Overview (330)7.1.1Plug-in Basics (330)7.1.2First Plug-in Slot of Sounds: Choosing the Sound’s Role (334)7.1.3Loading, Removing, and Replacing a Plug-in (335)7.1.3.1Browser Plug-in Slot Selection (341)7.1.4Adjusting the Plug-in Parameters (344)7.1.5Bypassing Plug-in Slots (344)7.1.6Using Side-Chain (346)7.1.7Moving Plug-ins (346)7.1.8Alternative: the Plug-in Strip (348)7.1.9Saving and Recalling Plug-in Presets (348)7.1.9.1Saving Plug-in Presets (349)7.1.9.2Recalling Plug-in Presets (350)7.1.9.3Removing a Default Plug-in Preset (351)7.2The Sampler Plug-in (352)7.2.1Page 1: Voice Settings / Engine (354)7.2.2Page 2: Pitch / Envelope (356)7.2.3Page 3: FX / Filter (359)7.2.4Page 4: Modulation (361)7.2.5Page 5: LFO (363)7.2.6Page 6: Velocity / Modwheel (365)7.3Using Native Instruments and External Plug-ins (367)7.3.1Opening/Closing Plug-in Windows (367)7.3.2Using the VST/AU Plug-in Parameters (370)7.3.3Setting Up Your Own Parameter Pages (371)7.3.4Using VST/AU Plug-in Presets (376)7.3.5Multiple-Output Plug-ins and Multitimbral Plug-ins (378)8Using the Audio Plug-in (380)8.1Loading a Loop into the Audio Plug-in (384)8.2Editing Audio in the Audio Plug-in (385)8.3Using Loop Mode (386)8.4Using Gate Mode (388)9Using the Drumsynths (390)9.1Drumsynths – General Handling (391)9.1.1Engines: Many Different Drums per Drumsynth (391)9.1.2Common Parameter Organization (391)9.1.3Shared Parameters (394)9.1.4Various Velocity Responses (394)9.1.5Pitch Range, Tuning, and MIDI Notes (394)9.2The Kicks (395)9.2.1Kick – Sub (397)9.2.2Kick – Tronic (399)9.2.3Kick – Dusty (402)9.2.4Kick – Grit (403)9.2.5Kick – Rasper (406)9.2.6Kick – Snappy (407)9.2.7Kick – Bold (409)9.2.8Kick – Maple (411)9.2.9Kick – Push (412)9.3The Snares (414)9.3.1Snare – Volt (416)9.3.2Snare – Bit (418)9.3.3Snare – Pow (420)9.3.4Snare – Sharp (421)9.3.5Snare – Airy (423)9.3.6Snare – Vintage (425)9.3.7Snare – Chrome (427)9.3.8Snare – Iron (429)9.3.9Snare – Clap (431)9.3.10Snare – Breaker (433)9.4The Hi-hats (435)9.4.1Hi-hat – Silver (436)9.4.2Hi-hat – Circuit (438)9.4.3Hi-hat – Memory (440)9.4.4Hi-hat – Hybrid (442)9.4.5Creating a Pattern with Closed and Open Hi-hats (444)9.5The Toms (445)9.5.1Tom – Tronic (447)9.5.2Tom – Fractal (449)9.5.3Tom – Floor (453)9.5.4Tom – High (455)9.6The Percussions (456)9.6.1Percussion – Fractal (458)9.6.2Percussion – Kettle (461)9.6.3Percussion – Shaker (463)9.7The Cymbals (467)9.7.1Cymbal – Crash (469)9.7.2Cymbal – Ride (471)10Using the Bass Synth (474)10.1Bass Synth – General Handling (475)10.1.1Parameter Organization (475)10.1.2Bass Synth Parameters (477)11Working with Patterns (479)11.1Pattern Basics (479)11.1.1Pattern Editor Overview (480)11.1.2Navigating the Event Area (486)11.1.3Following the Playback Position in the Pattern (488)11.1.4Jumping to Another Playback Position in the Pattern (489)11.1.5Group View and Keyboard View (491)11.1.6Adjusting the Arrange Grid and the Pattern Length (493)11.1.7Adjusting the Step Grid and the Nudge Grid (497)11.2Recording Patterns in Real Time (501)11.2.1Recording Your Patterns Live (501)11.2.2The Record Prepare Mode (504)11.2.3Using the Metronome (505)11.2.4Recording with Count-in (506)11.2.5Quantizing while Recording (508)11.3Recording Patterns with the Step Sequencer (508)11.3.1Step Mode Basics (508)11.3.2Editing Events in Step Mode (511)11.3.3Recording Modulation in Step Mode (513)11.4Editing Events (514)11.4.1Editing Events with the Mouse: an Overview (514)11.4.2Creating Events/Notes (517)11.4.3Selecting Events/Notes (518)11.4.4Editing Selected Events/Notes (526)11.4.5Deleting Events/Notes (532)11.4.6Cut, Copy, and Paste Events/Notes (535)11.4.7Quantizing Events/Notes (538)11.4.8Quantization While Playing (540)11.4.9Doubling a Pattern (541)11.4.10Adding Variation to Patterns (541)11.5Recording and Editing Modulation (546)11.5.1Which Parameters Are Modulatable? (547)11.5.2Recording Modulation (548)11.5.3Creating and Editing Modulation in the Control Lane (550)11.6Creating MIDI Tracks from Scratch in MASCHINE (555)11.7Managing Patterns (557)11.7.1The Pattern Manager and Pattern Mode (558)11.7.2Selecting Patterns and Pattern Banks (560)11.7.3Creating Patterns (563)11.7.4Deleting Patterns (565)11.7.5Creating and Deleting Pattern Banks (566)11.7.6Naming Patterns (568)11.7.7Changing the Pattern’s Color (570)11.7.8Duplicating, Copying, and Pasting Patterns (571)11.7.9Moving Patterns (574)11.7.10Adjusting Pattern Length in Fine Increments (575)11.8Importing/Exporting Audio and MIDI to/from Patterns (576)11.8.1Exporting Audio from Patterns (576)11.8.2Exporting MIDI from Patterns (577)11.8.3Importing MIDI to Patterns (580)12Audio Routing, Remote Control, and Macro Controls (589)12.1Audio Routing in MASCHINE (590)12.1.1Sending External Audio to Sounds (591)12.1.2Configuring the Main Output of Sounds and Groups (596)12.1.3Setting Up Auxiliary Outputs for Sounds and Groups (601)12.1.4Configuring the Master and Cue Outputs of MASCHINE (605)12.1.5Mono Audio Inputs (610)12.1.5.1Configuring External Inputs for Sounds in Mix View (611)12.2Using MIDI Control and Host Automation (614)12.2.1Triggering Sounds via MIDI Notes (615)12.2.2Triggering Scenes via MIDI (622)12.2.3Controlling Parameters via MIDI and Host Automation (623)12.2.4Selecting VST/AU Plug-in Presets via MIDI Program Change (631)12.2.5Sending MIDI from Sounds (632)12.3Creating Custom Sets of Parameters with the Macro Controls (636)12.3.1Macro Control Overview (637)12.3.2Assigning Macro Controls Using the Software (638)12.3.3Assigning Macro Controls Using the Controller (644)13Controlling Your Mix (646)13.1Mix View Basics (646)13.1.1Switching between Arrange View and Mix View (646)13.1.2Mix View Elements (647)13.2The Mixer (649)13.2.1Displaying Groups vs. Displaying Sounds (650)13.2.2Adjusting the Mixer Layout (652)13.2.3Selecting Channel Strips (653)13.2.4Managing Your Channels in the Mixer (654)13.2.5Adjusting Settings in the Channel Strips (656)13.2.6Using the Cue Bus (660)13.3The Plug-in Chain (662)13.4The Plug-in Strip (663)13.4.1The Plug-in Header (665)13.4.2Panels for Drumsynths and Internal Effects (667)13.4.3Panel for the Sampler (668)13.4.4Custom Panels for Native Instruments Plug-ins (671)13.4.5Undocking a Plug-in Panel (Native Instruments and External Plug-ins Only) (675)13.5Controlling Your Mix from the Controller (677)13.5.1Navigating Your Channels in Mix Mode (678)13.5.2Adjusting the Level and Pan in Mix Mode (679)13.5.3Mute and Solo in Mix Mode (680)13.5.4Plug-in Icons in Mix Mode (680)14Using Effects (681)14.1Applying Effects to a Sound, a Group or the Master (681)14.1.1Adding an Effect (681)14.1.2Other Operations on Effects (690)14.1.3Using the Side-Chain Input (692)14.2Applying Effects to External Audio (695)14.2.1Step 1: Configure MASCHINE Audio Inputs (695)14.2.2Step 2: Set up a Sound to Receive the External Input (698)14.2.3Step 3: Load an Effect to Process an Input (700)14.3Creating a Send Effect (701)14.3.1Step 1: Set Up a Sound or Group as Send Effect (702)14.3.2Step 2: Route Audio to the Send Effect (706)14.3.3 A Few Notes on Send Effects (708)14.4Creating Multi-Effects (709)15Effect Reference (712)15.1Dynamics (713)15.1.1Compressor (713)15.1.2Gate (717)15.1.3Transient Master (721)15.1.4Limiter (723)15.1.5Maximizer (727)15.2Filtering Effects (730)15.2.1EQ (730)15.2.2Filter (733)15.2.3Cabinet (737)15.3Modulation Effects (738)15.3.1Chorus (738)15.3.2Flanger (740)15.3.3FM (742)15.3.4Freq Shifter (743)15.3.5Phaser (745)15.4Spatial and Reverb Effects (747)15.4.1Ice (747)15.4.2Metaverb (749)15.4.3Reflex (750)15.4.4Reverb (Legacy) (752)15.4.5Reverb (754)15.4.5.1Reverb Room (754)15.4.5.2Reverb Hall (757)15.4.5.3Plate Reverb (760)15.5Delays (762)15.5.1Beat Delay (762)15.5.2Grain Delay (765)15.5.3Grain Stretch (767)15.5.4Resochord (769)15.6Distortion Effects (771)15.6.1Distortion (771)15.6.2Lofi (774)15.6.3Saturator (775)15.7Perform FX (779)15.7.1Filter (780)15.7.2Flanger (782)15.7.3Burst Echo (785)15.7.4Reso Echo (787)15.7.5Ring (790)15.7.6Stutter (792)15.7.7Tremolo (795)15.7.8Scratcher (798)16Working with the Arranger (801)16.1Arranger Basics (801)16.1.1Navigating Song View (804)16.1.2Following the Playback Position in Your Project (806)16.1.3Performing with Scenes and Sections using the Pads (807)16.2Using Ideas View (811)16.2.1Scene Overview (811)16.2.2Creating Scenes (813)16.2.3Assigning and Removing Patterns (813)16.2.4Selecting Scenes (817)16.2.5Deleting Scenes (818)16.2.6Creating and Deleting Scene Banks (820)16.2.7Clearing Scenes (820)16.2.8Duplicating Scenes (821)16.2.9Reordering Scenes (822)16.2.10Making Scenes Unique (824)16.2.11Appending Scenes to Arrangement (825)16.2.12Naming Scenes (826)16.2.13Changing the Color of a Scene (827)16.3Using Song View (828)16.3.1Section Management Overview (828)16.3.2Creating Sections (833)16.3.3Assigning a Scene to a Section (834)16.3.4Selecting Sections and Section Banks (835)16.3.5Reorganizing Sections (839)16.3.6Adjusting the Length of a Section (840)16.3.6.1Adjusting the Length of a Section Using the Software (841)16.3.6.2Adjusting the Length of a Section Using the Controller (843)16.3.7Clearing a Pattern in Song View (843)16.3.8Duplicating Sections (844)16.3.8.1Making Sections Unique (845)16.3.9Removing Sections (846)16.3.10Renaming Scenes (848)16.3.11Clearing Sections (849)16.3.12Creating and Deleting Section Banks (850)16.3.13Working with Patterns in Song view (850)16.3.13.1Creating a Pattern in Song View (850)16.3.13.2Selecting a Pattern in Song View (850)16.3.13.3Clearing a Pattern in Song View (851)16.3.13.4Renaming a Pattern in Song View (851)16.3.13.5Coloring a Pattern in Song View (851)16.3.13.6Removing a Pattern in Song View (852)16.3.13.7Duplicating a Pattern in Song View (852)16.3.14Enabling Auto Length (852)16.3.15Looping (853)16.3.15.1Setting the Loop Range in the Software (854)16.4Playing with Sections (855)16.4.1Jumping to another Playback Position in Your Project (855)16.5Triggering Sections or Scenes via MIDI (856)16.6The Arrange Grid (858)16.7Quick Grid (860)17Sampling and Sample Mapping (862)17.1Opening the Sample Editor (862)17.2Recording Audio (863)17.2.1Opening the Record Page (863)17.2.2Selecting the Source and the Recording Mode (865)17.2.3Arming, Starting, and Stopping the Recording (868)17.2.5Using the Footswitch for Recording Audio (871)17.2.6Checking Your Recordings (872)17.2.7Location and Name of Your Recorded Samples (876)17.3Editing a Sample (876)17.3.1Using the Edit Page (877)17.3.2Audio Editing Functions (882)17.4Slicing a Sample (890)17.4.1Opening the Slice Page (891)17.4.2Adjusting the Slicing Settings (893)17.4.3Live Slicing (898)17.4.3.1Live Slicing Using the Controller (898)17.4.3.2Delete All Slices (899)17.4.4Manually Adjusting Your Slices (899)17.4.5Applying the Slicing (906)17.5Mapping Samples to Zones (912)17.5.1Opening the Zone Page (912)17.5.2Zone Page Overview (913)17.5.3Selecting and Managing Zones in the Zone List (915)17.5.4Selecting and Editing Zones in the Map View (920)17.5.5Editing Zones in the Sample View (924)17.5.6Adjusting the Zone Settings (927)17.5.7Adding Samples to the Sample Map (934)18Appendix: Tips for Playing Live (937)18.1Preparations (937)18.1.1Focus on the Hardware (937)18.1.2Customize the Pads of the Hardware (937)18.1.3Check Your CPU Power Before Playing (937)18.1.4Name and Color Your Groups, Patterns, Sounds and Scenes (938)18.1.5Consider Using a Limiter on Your Master (938)18.1.6Hook Up Your Other Gear and Sync It with MIDI Clock (938)18.1.7Improvise (938)18.2Basic Techniques (938)18.2.1Use Mute and Solo (938)18.2.2Use Scene Mode and Tweak the Loop Range (939)18.2.3Create Variations of Your Drum Patterns in the Step Sequencer (939)18.2.4Use Note Repeat (939)18.2.5Set Up Your Own Multi-effect Groups and Automate Them (939)18.3Special Tricks (940)18.3.1Changing Pattern Length for Variation (940)18.3.2Using Loops to Cycle Through Samples (940)18.3.3Using Loops to Cycle Through Samples (940)18.3.4Load Long Audio Files and Play with the Start Point (940)19Troubleshooting (941)19.1Knowledge Base (941)19.2Technical Support (941)19.3Registration Support (942)19.4User Forum (942)20Glossary (943)Index (951)1Welcome to MASCHINEThank you for buying MASCHINE!MASCHINE is a groove production studio that implements the familiar working style of classi-cal groove boxes along with the advantages of a computer based system. MASCHINE is ideal for making music live, as well as in the studio. It’s the hands-on aspect of a dedicated instru-ment, the MASCHINE hardware controller, united with the advanced editing features of the MASCHINE software.Creating beats is often not very intuitive with a computer, but using the MASCHINE hardware controller to do it makes it easy and fun. You can tap in freely with the pads or use Note Re-peat to jam along. Alternatively, build your beats using the step sequencer just as in classic drum machines.Patterns can be intuitively combined and rearranged on the fly to form larger ideas. You can try out several different versions of a song without ever having to stop the music.Since you can integrate it into any sequencer that supports VST, AU, or AAX plug-ins, you can reap the benefits in almost any software setup, or use it as a stand-alone application. You can sample your own material, slice loops and rearrange them easily.However, MASCHINE is a lot more than an ordinary groovebox or sampler: it comes with an inspiring 7-gigabyte library, and a sophisticated, yet easy to use tag-based Browser to give you instant access to the sounds you are looking for.What’s more, MASCHINE provides lots of options for manipulating your sounds via internal ef-fects and other sound-shaping possibilities. You can also control external MIDI hardware and 3rd-party software with the MASCHINE hardware controller, while customizing the functions of the pads, knobs and buttons according to your needs utilizing the included Controller Editor application. We hope you enjoy this fantastic instrument as much as we do. Now let’s get go-ing!—The MASCHINE team at Native Instruments.MASCHINE Documentation1.1MASCHINE DocumentationNative Instruments provide many information sources regarding MASCHINE. The main docu-ments should be read in the following sequence:1.MASCHINE Getting Started: This document provides a practical approach to MASCHINE viaa set of tutorials covering easy and more advanced tasks in order to help you familiarizeyourself with MASCHINE.2.MASCHINE Manual (this document): The MASCHINE Manual provides you with a compre-hensive description of all MASCHINE software and hardware features.Additional documentation sources provide you with details on more specific topics:▪Controller Editor Manual: Besides using your MASCHINE hardware controller together withits dedicated MASCHINE software, you can also use it as a powerful and highly versatileMIDI controller to pilot any other MIDI-capable application or device. This is made possibleby the Controller Editor software, an application that allows you to precisely define all MIDIassignments for your MASCHINE controller. The Controller Editor was installed during theMASCHINE installation procedure. For more information on this, please refer to the Con-troller Editor Manual available as a PDF file via the Help menu of Controller Editor.▪Online Support Videos: You can find a number of support videos on The Official Native In-struments Support Channel under the following URL: https:///NIsupport-EN. We recommend that you follow along with these instructions while the respective ap-plication is running on your computer.Other Online Resources:If you are experiencing problems related to your Native Instruments product that the supplied documentation does not cover, there are several ways of getting help:▪Knowledge Base▪User Forum▪Technical Support▪Registration SupportYou will find more information on these subjects in the chapter Troubleshooting.1.2Document ConventionsThis section introduces you to the signage and text highlighting used in this manual. This man-ual uses particular formatting to point out special facts and to warn you of potential issues. The icons introducing these notes let you see what kind of information is to be expected:This document uses particular formatting to point out special facts and to warn you of poten-tial issues. The icons introducing the following notes let you see what kind of information can be expected:Furthermore, the following formatting is used:▪Text appearing in (drop-down) menus (such as Open…, Save as… etc.) in the software and paths to locations on your hard disk or other storage devices is printed in italics.▪Text appearing elsewhere (labels of buttons, controls, text next to checkboxes etc.) in the software is printed in blue. Whenever you see this formatting applied, you will find the same text appearing somewhere on the screen.▪Text appearing on the displays of the controller is printed in light grey. Whenever you see this formatting applied, you will find the same text on a controller display.▪Text appearing on labels of the hardware controller is printed in orange. Whenever you see this formatting applied, you will find the same text on the controller.▪Important names and concepts are printed in bold.▪References to keys on your computer’s keyboard you’ll find put in square brackets (e.g.,“Press [Shift] + [Enter]”).►Single instructions are introduced by this play button type arrow.→Results of actions are introduced by this smaller arrow.Naming ConventionThroughout the documentation we will refer to MASCHINE controller (or just controller) as the hardware controller and MASCHINE software as the software installed on your computer.The term “effect” will sometimes be abbreviated as “FX” when referring to elements in the MA-SCHINE software and hardware. These terms have the same meaning.Button Combinations and Shortcuts on Your ControllerMost instructions will use the “+” sign to indicate buttons (or buttons and pads) that must be pressed simultaneously, starting with the button indicated first. E.g., an instruction such as:“Press SHIFT + PLAY”means:1.Press and hold SHIFT.2.While holding SHIFT, press PLAY and release it.3.Release SHIFT.Unlabeled Buttons on the ControllerThe buttons and knobs above and below the displays on your MASCHINE controller do not have labels.。

热量控制系统设计手册说明书

热量控制系统设计手册说明书

The Design of Temperature Control System for Rice Wine FermentationZHANG Shengyi and WANG Xinming,HuBei Engineering University of School of Physics and Electronic Information Engineering, Xiaogan,Hubei, ChinaKeywords: Fermentation temperature; STM32; control system; temperature control moduleAbstract:Fermentation temperature is the key to decide the quality of the rice wine, so the temperature controlling system in fermentation room is established base on stm32 microcontroller and digital temperature sensor. The whole block diagram for the system is firstly detailed, and then the Temperature collecting module and temperature control module are also described. At last the software flow chart is discussed. The experiment is done based on designed system, and the data is analyzed. The result show that designed system can realize high accuracy temperature controlling.IntroductionsFermentation technology is one of the important processes in the rice wine production and Fermentation temperature is the key to decide the quality of the rice wine [1] [2]. If the fermentation temperature is controlled within desired environment, the needed quantity for material could be reduced and the quality of the rice wine could be greatly improved. Face to the increment of the production, the conventional manual temperature controlling encounters a lot of difficulty [3] [4] [5]. In contrast, the automatic control of by means of microcontroller, digital sensor and some implement part can be widely used in the process of fermentation.According to above description, the temperature control system is designed and some experiment is done. In this paper, the temperature control system is firstly detailed, including whole block diagram for the system, the control core STM32F103, Temperature collecting module, the drive circuit for the temperature control module and software flow chart designs. Then, the experiment is done based on designed system. At last, the data is analyzed and some conclusion is derived.The design for temperature control systemThe whole block diagram for the system. The system block diagram for the control system with the control core of STM32F103 controller is shown in figure 1. It is consisted of temperature collecting module, temperature control module and MCU minimum system. The sensor for temperature collecting module is DS18B20, with the character of 1-Wire interface in which all of the data, address and command can be transmitted. Temperature control module is consisted of the heating part and cooling part, it is separately electric incandescent lamp and fans. The system except MCU minimum system is mounted inside the fermentation room.In this system, the temperature of the fermentation room can be real-time collected by the sensor and sent to microcontroller, if the temperature is above setting value, the fans should be startup; otherwise, electric incandescent lamp is lightened. Further, the FLASH, SRAM andkeyboard is expandedFig.1 the system block diagram for the control systemThe Temperature collecting module. The temperature collecting sensor in this paper is the Digital Thermometer DS18B20 Which provides 9 to 12-bit temperature readings [6] [7]. Because of the Information sent to/from the DS18B20 over a 1-Wire interface, only one wire (and ground) needs to be connected from a central microprocessor to a DS18B20. Power for reading, writing, and performing temperature conversions can be derived from the data line itself with no need for an external power source.PFig.2 diagrammatic sketch Wire Connected between sensor and microcontroller Because each DS18B20 contains a unique silicon serial number, multiple DS18B20s can exist on the same 1-Wire bus. This allows for placing temperature sensors in many different places. Applications where this feature is useful include HV AC environmental controls, sensing temperatures inside buildings, equipment or machinery, and process monitoring and control.The drive circuit for the temperature control module. The drive circuit of temperature control module is illustrated in figure 3, the electric incandescent lamp and fans is drive by 220 AVC, while theirs control is finished through relay K1 and K2. Because it need large current for driving of relay K1 and K2, the ULN2003 with high voltage and high current darlington pairs is adopted. The control command of lamp and fans is separately input from channel of IN1 and IN2 of ULN2003, these signal is enlarged and drive the relay action.Fig.3 The circuit of temperature control moduleFig. 4 the flow chart for the temperature control system of Fermentation room Software designs for the designed system. The flow chart of the system software is illustrated in figure 4. When the power supply is switched on, the system will enter into initial state. If the new temperature range of the fermentation room is set, the current temperature is collected and it enters into switch select. If the current value is less than setting range, the hearting module is started and the cooling module is stopped; if the current value is more than setting range, the hearting module is stopped and the cooling module is started; otherwise, this system should be maintained current status.Experiment and resultAt last, the temperature control experiment in fermentation room is done with the same initial indoor temperature of 20℃. Because of the perfect fermentation temperature is 28-32℃, so the five different setting temperature of 28℃, 29℃, 30℃, 31℃ and 32℃ is selected for experiment, both the temperature after adjusted and the time consumption for temperature control are recorded the experimental result for temperature control is shown in table 1.Tab. 1 experimental result for temperature controlInitial value(℃) preset value(℃) Adjusted value(℃) Adjust time(s)20 28 28.4 10120 29 28.8 10320 30 29.8 10420 31 31.1 10320 32 31.8 102From the table, the temperature after adjusted is near is setting value, and within permissible error and the time consumption is almost same. So we can infer that the designed system can reach high accuracy temperature controlling and it reaches desired function.ConclusionsTo achieve high accuracy temperature controlling for rice wine fermentation room, the experiment is founded through temperature collecting module, temperature control module and MCU minimum system. Based on designed system, the experiment is done, and the result shows that designed system can realize high accuracy temperature controlling.References[1] Zhu Y, Zhang J, Shi Z, Mao Z. Optimization of operating conditions in rice heat blast process for Chinese rice wine production by combinational utilization of neural network and genetic algorithms. J Inst Brew, 2004,110:117–123[2] Gohel V, Duan G. Conventional process for ethanol production from Indian broken rice and pearl millet. Bioprocess Biosyst Eng ,2012, 35:1297–1308[3] Wang J, Zhang Y, Yu Q . Determination of alcohol and total acid content in Miaofu rice wine by near infrared spectroscopy. China Brewing ,2011,11:168–170[4] Mo X, Xu Y, Fan W. Characterization of aroma compounds in Chinese rice wine Qu by solvent-assisted flavor evaporation and headspace solid-phase microextraction. J Agric Food Chem,2010, 58:2462–2469[5] Jin Y, Fan W, Xu Y, Zhao G. Research on the tolerance of yellow rice wine yeast. Liquor-Mak Sci and Technol,2008, 6:17–21[6] Gu ZY, Liu LY, Du ZH. DS18B20 C language programming interface. Microcontrollers Embeded Syst, 2002, 7:22–24[7] Liu JT, Mao SK. Principle of DS18B20 and its interface design based on C. Instrum Meters User, 2005,12(6):138–140。

南京大学20春《管理原理》第2次作业

南京大学20春《管理原理》第2次作业
B、planning
C、organizational culture
D、manufacturing design
E、directing
说明:
题号:17题型:单选题(请在以下几个选项中选择唯一正确答案)本题分数:2
The three components that make up an attitude are ______________.
A、managers
B、leaders
C、organizers
D、visionaries
E、team members.
说明:
题号:6题型:单选题(请在以下几个选项中选择唯一正确答案)本题分数:2
Of the following, which is NOT a common source of information used by managers to measure performance?
A、measuring actual performance
B、changing the standard
C、taking managerial action
D、comparing actual against the standard
说明:
题号:11题型:单选题(请在以下几个选项中选择唯一正确答案)本题分数:2
A、cognitive, affective, behavioral.
B、traits, behavioral, emotional.
C、knowledge, opinion, individual history.
D、intention, opinion, environment.
E、pre-opinion, experience,

唑虫酰胺的合成

唑虫酰胺的合成

CH2CH3COCH3 + (COOC2H5)2 C2H5ONa CH3CH2COCH2COCOOC2H5 NH2NH2 H2O
C2H5 N N H
C2H5
C2H5
Me2SO4
COOC2H5
Cl
N
SO2Cl2
N COOC2H5
CH3
C2H5
Cl
N N COOC2H5 CH3
1. NaOH 2. 酸化
2.2 中间体 4-(4-甲基苯氧基)苄胺(B)的合成
2.2.1 对氯苯甲腈的合成 2.2.1.1 氰化钾-氰化亚铜水溶液的制备
将 37.5 g 胆矾和 9.75 g 氯化钠溶于 100 ml 热水 中,配成溶液Ⅰ;将 7.95 g 亚硫酸氢钠和 5.25 g 氢 氧化钠溶于 45 ml 水中,配成溶液Ⅱ。将溶液Ⅱ缓 慢倒入溶液Ⅰ中,搅拌使之反应完全,生成白色沉 淀。冰浴条件下向溶液中加入 20.2 g 氰化钾,搅拌 得到无色透明溶液。 2.2.1.2 对氯苯胺重氮盐的制备
唑虫酰胺的通用名为 tolfenpyrad,商品名为 MATI-HATI,代号 OMI-88,化学名称为:N-[4-(4甲基苯氧基)苄基]-1-甲基-3-乙基-4-氯-5-吡唑甲酰 胺,结构式如下:
C2H5
Cl
N
N CONHCH2
O
CH3
CH3
其纯品为类白色固体粉末,密度 (25℃) :
1.18 g/cm3,蒸汽压 (25℃):< 5×10-7 Pa。溶解 度 (25℃):水 0.037 mg/L,正己烷 7.41 g/L,甲 苯 366 g/L,甲醇 59.6 g/L。分配系数 (正辛醇/水) (25℃):log Pow 5.61。
将 15.3 g (0.12 mol) 对氯苯胺溶于 17 ml 水中, 再滴加 24 ml 浓盐酸,冷却至 0~5℃下搅拌有白色 粒状晶体析出。同样的温度下滴加 33 g 25.9%的亚 硝酸钠水溶液,用淀粉-碘化钾试纸确定反应终点, 得到黄色溶液。再用固体碳酸钠粉末中和,搅拌下 保持温度在 0~5℃,备用。 2.2.1.3 对氯苯甲腈的制备

如何控制自己的情绪(Howtocontrolyouremotions)

如何控制自己的情绪(Howtocontrolyouremotions)

如何控制自己的情绪(How to control your emotions)Not good at controlling and regulating their emotions, great wrath, compassion, impatience, do things indiscriminately, regardless of the inferiority. Loneliness, frustration, learning, work efficiency decline.Main points:(L) vent the energy of bad emotions. For example, when you get angry, not hurried to other places, or with his fist hammer walls, or find a labourer one thousand, or run a lap, so you can put out the energy release due to anger, to calm down, or you might cry over pain. Field. Laughter is also a way of releasing energy and regulating the balance of the body.(2) rationally dispelling bad emotions. You must first admit the bad mood; secondly, that negative emotions exist after it is necessary to analyze the causes of this emotion, and figuring out why distressed, sad or angry, things that can help us understand their anguish, sorrow, anger, is indeed grim, worry, be angry, sometimes it is not so bad, the mood will be digested; finally, sometimes really grim, worry, anger reason, then, to seek appropriate methods and ways to solve it. For example, if you are not sure before the exam, you can test anxiety, you have to actively shift the energy to strengthen learning, focus on good review, reduce their worries.(3) forgetting or transferring bad emotions. In general, things that are strongly stimulated by one's emotions are usually related to one's own interests. It is very difficult to forget them very soon. But it can be actively transferred, that is,try to shift your mind to something more meaningful, or to volunteer to help others, or to talk to close friends, or to find useful books to read. Do not leave yourself in a state of mental emptiness and mental emptiness. When the unpleasant emotion is produced, the energy can be quickly transferred to the person who is in it, and the bad emotion will stay on him for a short time.(4) take the necessary methodsSelf encouragement. That is, to comfort oneself with the philosophy of life or some wise thought, and to encourage ourselves to struggle against pain and adversity. Self encouragement is one of the power source of human spirit, a person in the face of suffering, and against adversity, as long as they can effectively carry out self encouragement, he will feel the power, we can take heart in pain.Verbal suggestion. When you are depressed by the bad complex, you can adjust and relax the psychological tension by means of verbal suggestion, so as to relieve the bad mood. For example, when you're angry, you can use your words to say "don't be angry." anger will do things wrong". When you are in sorrow, remind yourself that "sorrow is useless, nothing is beneficial, or face the reality. Think about it.". "And so on, in the relaxation of calm, remove distracting thoughts, focus on the situation, this self suggestion, to improve the mood will be beneficial.Asking for guidance. Sometimes, it's not enough to adjust the bad mood alone, but also need help from others. Psychologicalresearch believes that when people's psychology is depressed, it should be allowed to vent, and some of the anguish in the heart dumped. Therefore, when young people have depression, they can take the initiative to find their relatives and friends, tell their inner sorrow, so as to get rid of unhealthy emotions.Environmental regulation method. Environment also plays an important role in the emotion and emotion of human beings. Elegant and tidy the room, bright light, color and soft environment, make people produce a quiet, relaxed mood. On the contrary, dark, narrow, dirty environment, bring suffocating and unpleasant emotions. Therefore, to change the environment, can also play a role in regulating emotions, when you are in bad mood and depression, may wish to walk outside to see the beauty, the beauty of nature, be broad-minded mind,Physical and mental pleasure, has a good effect on the regulation of human mental activity.When a person is in a state of bad mood, he can often adjust his emotion by the following methods:(1) conscious regulation of legal person consciousness can regulate the occurrence and intensity of emotion, and some people with high level of ideological training are more likely to adjust their emotions than those with lower level ofself-cultivation. One should try to control the change of emotion with consciousness...... "I can."...... Add to what you want to do to control your emotions.(2) language is a powerful tool for the emotional experienceof a person. Language can cause or inhibit emotional responses, even if the silent internal language can also play a regulatory role. Lin Zexu hung on the wall "anger" two words scroll, this is to use language to control the mood of a good way.(3) attention shifting method shifts attention from negative emotions to meaningful directions. When people depressed, worry, look at emotional film, read the Memoirs of Du can receive good results.(4) action transfer method to overcome some long-term negative emotions, can use new work, new action to transfer negative emotional interference. Beethoven used to join the army to overcome the pain of lovelorn, it may be a good choice. The biggest psychological suffering is the biggest burden of worry about personal gains and losses; spiritual shackles than fame. People can not blindly pursue fame and wealth, but also can not be lack of ambition and struggle spirit. Health first heart, heart light fame. Contentment, physical and mental health. Art Master Mr. Liu Meisu has over 90, still fresh, brush freely. The secret of longevity is "unmoved either by gain or loss, see pretrial blossom; fate not, hope heaven yunjuanyunshu. "One learns to be optimistic, indifferent to fame and gain, to maintain healthy mood, and that fate is always in his own hands.".Anger of the masters of mood, when hi hi, when sadness is sad. When angry happens, is there any reason to be angry, and what is the consequence of two thoughts? So you can become calm and emotionally stable.Try to increase positive emotions. There are three methods: one is more friends, fun in group communication; two is focotex small target, small target is easy to implement, each implementation can bring pleasure satisfaction; the three is to learn the dialectical thinking, people can easily treat setbacks and failures.Humor often smiles and more humor. Psychologists believe that people laugh not because they are happy, but because they are happy. It's not because of sorrow that makes you cry, it's because of crying. Laugh more in your life.Helping people learn Lei Feng to do good can bring happiness to others, but also make himself feel at ease, his mood is calm, and has a good sense of security.Catharsis meets unpleasant and unpleasant things, through sports, reading novels, listening to music, watching movies, looking for friends to talk to vent their unpleasant feelings, you can also cry.Compensatory transfer can be used to compensate for another need when the demand is blocked or frustrated. This course is not good, you can strive for good results in another class, but also by distracting attention, change the environment to divert the emotional direction.Sublimation is to restore the bad emotions to the sublime realm. Such as the famous writer Gerd in after the breakup, the lovelorn emotional energy sublimation to literary writing, wrote the famous "" the sorrows of Young Werther ".Relax in a bad mood, can through the top-down step by step to relax the body, or through self hypnosis, self massage and other ways to make himself into a relaxed static state, and then with a smile, imagination has experienced the happy situation, in order to eliminate bad mood.What foods mediate emotions?Over the years, studies have shown that certain foods can affect the production of certain chemicals in the brain, thereby improving people's mood.Total amino acids in whole wheat bread can increase the level of 5 serotonin in the brain and make people feel happy. And whole wheat bread helps to absorb tryptophan. Before eating protein rich meat, cheese and other food, eat a few slices of whole wheat bread, can guarantee the tryptophan into the brain, not being squeezed out of other amino acids.Coffee in the morning has a refreshing effect on a cup of coffee. Caffeine can temporarily cause blood pressure to rise slightly and block the chemicals that cause drowsiness. But drinking more than 3 cups a day may make you irritable and irritable.Water should drink enough water every day to prevent water shortages. You can't use coffee or other coffee drinks instead.Banana tension is closely related to magnesium deficiency, so busy people should supplement magnesium rich foods, such as bananas.Oranges and grapes, 150 mg daily dose of vitamin C (about two oranges), can make nervousness, irritability, depression bad mood improved.Capsaicin in chili peppers stimulates oral nerve endings and releases endorphins from the brain. This substance can cause temporary pleasure.Many chocolate women, especially when they are plagued by premenstrual syndrome or bad mood, particularly crave chocolate. Because chocolate has a calming effect.In order to reduce cholesterol completely avoid beef beef, often caused by iron deficiency, make people feel tired, depressed mood. Tests show that people who eat 3 ounces of beef a day can absorb more than 50% of the total calories of a person who is a vegetarian.Ancient oriental medicine believes that color has the unique ability to treat the human body and spirit.Ancient medicine believes that each person's character is unique, everyone has their favorite color, the depth of color also have particular emphasis. Ancient medical scientists established a reasonable system for revealing the different effects of different colors on human organism, which was established on the basis of careful study of the characteristics of each color. Ancient oriental medicine has a cure for the human body with the color of the rainbow.White: can play the role of consolidating and purifying the human body. If you match it with other colors, you can enhance the therapeutic effect of this color, so it's also a synergist for other colors. This is also an important reason for choosing white in hospital wards.Black: it can calm the emotional person and make the conflict restrained. But too much black leads to mental depression. Black and white collocation, the effect is particularly good. It can make people's mood peaceful, help the behavior of the controller, grasp the situation correctly. This is probably the reason why most people choose black clothes on the formal occasions such as politics, commercial stage and festival celebration.Red: it can stimulate human power, and it is the symbol of passion and desire. In people under the menstruation, hypotension, anemia, arthritis and high fever, pain, often advised them to touch the shades of red. There are some very funny things, the ancients in erysipelas arthritis, often with red cloth tied red place; children suffering from measles and chickenpox, witch doctor advice for them to wear red clothes. Superstition is a red cloth to avoid evil spirits. In fact, not a red cloth to ward off evil spirits, but red itself has a therapeutic effect.Orange: will stimulate people's communicative ability and good nature, will make life better. But people with too much mental activity should wear orange and blue clothes. Orange is an excellent color for treating depression.Yellow: like orange, it's also a mood modifier. It can help people to continue the good mental state, promote appetite, and is conducive to the operation of gastrointestinal function.Green: any kind of green is the symbol of sympathy, peace and relaxation. In the forest, surrounded by green leaves, you will feel relaxed and comfortable. Walking on the soft grass, you will feel very happy. Green can relieve physical and mental fatigue, stable blood pressure, headaches, eye fatigue and removal of red blood,It also helps fight cardiovascular disease. But people who suffer from cancer shouldn't wear green because they can stimulate the growth of tumors. Similarly, people with gallstones should try to wear less green clothes as much as possible.Blue: can play antibacterial role, can help the treatment of sore throat and respiratory diseases. Light blue can stimulate people's inspiration, help people sober awareness of themselves, so that people find a way out in loneliness. Dark blue can inspire people's will.Dian Qing (dark blue): an organ that helps heal the face and head: eyes, ears, and nose. Remember, this color is very active and can keep people energetic. However, indigo too much will make people easy to suffer from depression or sadness.Purple: is responsible for the human skeleton health, it helps to inhibit tumor growth, relieve joint pain, conducive to sleep. But improper use of purple can make people sleepy. If you planta plant in a room full of purple, it grows very slowly and often dies.Various color characteristics constitute the basic treatment of each color trend, but the depth of color is also worth noting. Brown is not the color of a rainbow, but it has long been called common sense color, and it can disturb the moods of people with a healthy mind. If people use too much grey, they feel sad, dull and indifferent. As we all know, yellow can stimulate people's appetite; dark blue can greatly reduce the appetite of bulimia people; green is conducive to food digestion, overcome intestinal diseases, and help to treat chronic diseases。

光子晶体结构生色纺织品的快速制备及其性能表征

光子晶体结构生色纺织品的快速制备及其性能表征

浙江理工大学学报,2021,45(2): 157-163Journal of Zhejiang Sci-Tech UniversityDOI:10. 3969/j.issn.l673-3851(n).2021. 02.001光子晶体结构生色纺织品的快速制备及其性能表征高雅芳%张耘箫',刘国金%周岚h,柴丽琴b,邵建,陈建勇15(浙江理工大学,a.浙江省纤维材料和加工技术研究重点实验室;b.先进纺织材料与制备技术教育部重点实验室,杭州310018)摘要:以聚(苯乙烯-甲基丙烯酸)(P(St-MAA))胶体微球为结构基元,利用喷涂法在黑色涤纶织物上快速制 备光子晶体结构生色薄膜。

通过控制预组装液质量浓度和喷涂距离,优化喷涂工艺参数,揭示肢体微球自组装过程 t结构色色相变化的机制,并分析制备所得光子晶体的光学性能。

结果表明:采用喷涂法制备光子晶体时,设定预 组装液质量浓度为30. 0%,喷涂距离为20 cm时,烘干时间为1min,可在织物表面快速得到明亮鲜艳的光子晶体结 构色;喷涂于织物表面的胶体微球在自组装过程中产生的一系列色彩变化,是由晶体中晶格间距不断缩小和晶体有 效折射率降低共同引起的;喷涂不同粒径股体微球自组装所得光子晶体均呈现出鲜艳的结构色效果,不同观察角度 下结构色色相不同,表现出明显的虹彩现象。

研究结果可为纺织品上快速制备仿生结构色提供理论依据。

关键词:涤纶;肢体微球;喷涂;光子晶体;结构色中图分类号:TS195. 5 文献标志码:A 文章编号:1673-3851 (2021) 03-0157-07Rapid preparation and characterization of chromogenictextiles with photonic crystal structureGAO Yafang" , ZHANG Yunxiaoa , LIU Guojina , ZHAO Lanb, CHAI Liqin b, SHAO Jianzhong", CHEN Jianyongh(a. Zhejiang Provincial Key Laboratory of Fiber Materials and Manufacturing Technology;b. Key Laboratory of Advanced Textile Materials and Manufacturing Technology,Ministry of Education, Zhejiang Sci-Tech University, Hangzhou 310018, China)Abstract:Chromogenic films with photonic crystal structure were rapidly prepared by spraying on black polyester fabrics with poly (styrene-methacrylic acid) (P(St-MAA)) colloidal microspheres as the structural motif. The parameters of spraying process were optimized, the mechanism of hue change of structural color during the self-assembly of colloidal microspheres was revealed, and the optical properties of the resulting photonic crystals were analyzed by controlling the mass concentration and spraying distance of the pre-assembly solution. The results indicated that when spraying method was used to prepare photonic crystals, the mass concentration of the pre-assembly solution was 30. 0%, the spraying distance was 20 cm and the drying time was 1min, bright photonic crystal structural color could be quickly obtained on the fabric surface. A series of color changes during the self-assembly of colloidal microspheres sprayed on the fabric surface were caused by the continuous reduction of lattice spacing in crystals and the decrease of effective refractive index of crystals. The photonic crystals obtained by the self-assembly of colloidal microspheres with different particle sizes showed bright structural colors, but the hues of structural colors were different under different viewing angles,which demonstrated an obvious iridescent收稿日期:2020—12—28 网络出版日期:2021—02—03基金项目:国家自然科学基金项目(52003242,51773181);浙江省自然科学基金项目(LQ19E030022,LY20E030006);浙江理工大学科研 启动基金项目(18012212-Y,19012134-Y)作者简介:高雅芳(1995 —),女,浙江绍兴人,硕土研究生,主要从事光子晶体结构生色方面的研究。

一、奖项类别自然科学奖

一、奖项类别自然科学奖

一、奖项类别:自然科学奖二、项目名称:集约旱作农田氮素循环机理与调控三、提名者及提名意见提名者:中国农学会提名意见:氮素是农业生产的关键元素。

理解农田氮素循环机理,是提高氮素增产效果并降低环境污染的理论基础。

该项目针对我国北方集约化旱作农田氮素利用率低、污染环境严重等突出问题,在土壤氮素转化特征、氧化亚氮(N2O)产生机制、氮肥去向及损失途径、推荐施氮量方法等相互联系的重要科学问题上,进行了长期系统的基础研究,取得了创新性成果。

揭示了我国北方集约化旱作农田土壤氮素转化特征,阐明了土壤硝态氮“持续累积与脉冲式淋洗”的机制。

发现铵态氮或酰胺态氮肥施入土壤后的强氨氧化过程导致亚硝态氮积累,进而引起土壤微域硝化细菌的反硝化作用是土壤N2O 产生的主要机制,提出了延缓强氨氧化过程是N2O减排的关键措施。

阐明了北方旱作农田氮肥去向和损失规律,发现残留肥料氮对土壤氮库的补偿是土壤氮素循环的重要环节,提出了“氮肥有效率”的概念和计算方法。

发现了集约化长期耕作农田在其他氮素输入和秸秆还田条件下,当季合理施氮量约等于作物地上部吸氮量的规律,提出并验证了基于目标产量和维持土壤氮素平衡的“理论施氮量”概念和计算方法。

完成了我国完整的活性氮来源和排放清单,揭示了农业面源污染严重的主要原因是氮素利用率和循环率低,为我国氮素综合管理和污染治理提供了科学基础。

8篇代表性论文总他引1223次,被SCI他引1015次,其中2篇被列入ESI 高被引论文。

成果受到国内外学术界高度关注的认可,获2018年度中国土壤学会科学技术一等奖。

提名该项目为国家自然科学奖二等奖。

四、项目简介氮素是农业生产的关键元素。

理解农田氮素循环过程和机理,是提高氮素增产效果并降低环境污染的理论基础,也是全球集约化农业研究的重要科学问题。

氮肥对我国粮食增产起到了十分重要的作用,但不合理施用又带来一系列环境污染问题。

该项目以我国北方集约旱作农田为研究对象,针对氮素投入高、利用率低、污染环境严重等突出问题,在土壤氮素转化特征与机理、氧化亚氮(N2O)产生机制、氮肥去向及损失途径、推荐施氮量方法等相互关联的重要科学问题上,进行了长期系统的基础研究,取得的创新性成果概括为以下四个方面。

接待国外客户常用英语

接待国外客户常用英语

问好1. Good morning/afternoon/evening. /May I help you? /Anything I can do for you?2. How do you do? /How are you? / Nice to meet you.3. It’s a great honor to meet you./I have been looking forward to meeting you.4. Welcome to China.5. We really wish you’d have a pleasant stay here.6. I hope you’ll have a pleasant stay here. Is this your fist visit to China?7. Do you have much trouble with jet lag?机场接客1. Excuse me; are you Mr. Wilson from the International Trading Corporation?2. How do I address you?3. My name is Benjamin liu. I’m from the Fuzhou E-fashion Electronic Company. I’m here to meet you.4. We have a car an over there to take you to you hotel. Did you have a nice trip?5. Mr. David smith asked me to come here in his place to pick you up.6. Do you need to get back your baggage?7. Is there anything you would like to do before we go to the hotel?相互介绍1. Let me introduce my self. My name is Benjamin Liu, an Int’l salesman in the Marketing Department.2. Hello, I am Benjamin Liu, an Int’l s alesman of FUZHOU E-FASHION ELECTRONIC COMPANY. Nice to meet you. /pleased to meet you. / It is a pleasure to meet you.3. I would like to introduce Mark Sheller, the Marketing department manager of our company.4. Let me introduce you to Mr. Li, general manager of our company.5. Mr. Smith, this is our General manage, Mr. Zhen, this is our Marketing Director, Mr.Lin. And this is our RD Department Manager, Mr. Wang.6. If I’m not mistaken, you must be Miss Chen from France.7. Do you remember me? Benjamin Liu from Marketing Department of PVC. We met several years ago.8. Is there anyone who has not been introduced yet?9. It is my pleasure to talk with you.10. Here is my business card. / May I give you my business card?11. May I have your business card? / Could you give me your business card?12. I am sorry. I can’t recall your name. / Could you tell me how to pronounce your name again?13. I’ am sorry. I have forgotten how to pronounce your name.小聊1. Is this your first time to China?2. Do you travel to China on business often?3. What kind of Chinese food do you like?4. What is the most interesting thing you have seen in China?5. What is surprising to your about China?6. The weather is really nice.7. What do you like to do in your spare time?8. What line of business are you in?9. What do you think about…? /What is your opinion?/What is your point of view?10. No wonder you're so experienced.11. It was nice to talking with you. / I enjoyed talking with you.12. Good. That's just what we want to hear.确认话意1. Could you say that again, please?2. Could you repeat that, please?3. Could you write that down?4. Could you speak a little more slowly, please?5. You mean…is that right?6. Do you mean..?7. Excuse me for interrupting you.社交招待1. Would like a glass of water? / can I get you a cup of Chinese red tea? / How about a Coke?2. All right, let me make some. I’ll be right back.3. A cup of coffee would be great. Thanks.4. There are many places where we can eat. How about Cantonese food?5. I would like to invite you for lunch today.6. Oh, I can’t let you pay. It is my treat, you are my guest.7. May I propose that we break for coffee now?8. Excuse me. I’ll be right back9. Excuse me a moment.告别1. Wish you a very pleasant journey home? Have a good journey!2. Thank you very much for everything you have done us during your stay in China.3. It is a pity you are leaving so soon.4. I’m looking forward to seeing you again.5. I’ll see you to the airport tomorrow morning.6. Don’t forget to look me up if you a…………re ever in FUZHOU. Have a nice journey!约会1. May I make an appointment? I‘d like to arrange a meeting to discuss our new order.2. Let’s fix the time and the place of our meeting.3. Can we make it a little later??4. Do you think you could make it Monday afternoon? That would suit me better.5. Would you please tell me when you are free?6. I’m afraid I have to cancel my appointment.7. It looks as if I won’t be able to keep the appointment we made.8. Will you change our appoint tomorrow at 10:00 to the day after tomorrow at the came time?9. Anytime except Monday would be all right.10. OK, I will be here, then.11. We'll leave some evenings free, that is, if it is all right with you.品质1. We have a very strict quality controlling system, which promises that goods we produced are always of the best quality.2. You have got the quality there as well as the style.3. How do you feel like the quality of our products?4. The high quality of the products will secure their leading status in the market place.5. You must be aware that our quality is far superior to others.6. We pride ourselves on quality. That is our best selling point.7. As long as the quality is good. It is all right if the price is a bit higher.8. They enjoy good reputation in the world.9. When we compare prices, we must first take into account the quality of the products.10. There is no quality problem. Quality is something we never neglect.11. You are right. It is good in material, fashionable in design, and superb in workmanship.12. We deliver all our orders within one month after receipt of the covering letters of credit.13. Do you have specific request for packing? Here are the samples of packing available now, you may have a look.14. I wonder if you have found that our specifications meet your requirements. I’m sure the prices we submitted are competitive. Sample Text1 I've come to make sure that your stay in Beijing is a pleasant one.我特地为你们安排使你们在北京的逗留愉快。

A novel way to fabricate tubular porous mullite membrane

A novel way to fabricate tubular porous mullite membrane

Available online atJournal of the European Ceramic Society33(2013)3249–3256A novel way to fabricate tubular porous mullite membrane supportsby TBA-based freezing casting methodRuiping Liu,Jie Yuan,Chang-an Wang∗School of Materials Science and Engineering,State Key Laboratory of New Ceramics and Fine Processing,Tsinghua University,Beijing100084,ChinaReceived27April2013;received in revised form29May2013;accepted2June2013Available online29June2013AbstractPorous tubular mullite supports with gradient unidirectional aligned pores were successfully fabricated by TBA-based freezing casting method. The effects of freezing temperature,solids loading and particle size distribution of mullite powders on the microstructure and properties of the supports were investigated extensively.The results show that the pore size,porosity and compressive strength of the supports can be effectively adjusted by controlling the parameters.Both the results of microstructure observations and properties testing indicate that the pore channel size increases along the freezing direction,accompanied by the changes of pore structure from homogeneous near the freezing medium to unidirectional away from the freezing medium.The pore channel size decreases significantly with increasing solids loading,decreasing freezing temperature and reducing the particle size.The porosity also decreases with increases of solids loading and freezing temperature,as well as reduces of the particle size,while the compressive strength increases.©2013Elsevier Ltd.All rights reserved.Keywords:Porous mullite tubes;Ceramic supports;Freezing casting;Unidirectional aligned pores;Gradient pore structure1.IntroductionIn recent decades,porous ceramic membranes have attracted increasing attention for their successful applications in many industry areas,such as wastewater treatment,1desalination,2gas separation process,3etc.Generally,only supported asymmetric ceramic membranes can be used in the practical applications due to their high separation selectivity,low permeation resis-tance and good mechanical performance.4The porous supports for membranous layer deposition play a key role by providing sufficient mechanical strength and various configurations,and can be prepared by several methods such as extrusion,5–7slip-casting,8and isostatic pressing.9Recently,the freeze-casting process has emerged as a candidate method for preparation of the porous ceramics,as it can produce interconnected pore chan-nels in a tailored manner,e.g.aligned pore channels on a scale of several microns,which will offer superior mechanical properties and higherflux.To date,water,10,11camphene12,13and tert-butyl alcohol(TBA)14have been successfully used as freezing vehi-cles.Of these,the unidirectional hexagonal pores can be formed ∗Corresponding author.Tel.:+861062785488;fax:+861062785488.E-mail address:wangca@(C.-a.Wang).by TBA sublimation,which will be favorable for the solid-liquidseparation process.15Most of the previous research has focused on the prepara-tion of traditional porous ceramic membrane supports by withseveral limited species such as alumina,16–20silicon carbide5,21and Si3N4.22However,both expensive starting materials andhigh sintering cost limit their extensive applications in moreindustrial separationfields,especially the massive pre-treatmentof solid-containing waste liquids or waste gases.As promisingstructural materials,mullite(3Al2O3·2SiO2)and mullite-based ceramics have been studied considerably in the last decades forits interesting properties,such as relatively low thermal expan-sion co-efficient,low specific gravity,high creep resistance,lowthermal conductivity,good infrared transparency and low dielec-tric constant.23,24Due to low thermal expansion coefficient,mullite-based ceramics with good thermal shock resistance arewidely applied in high-temperature thermal cycling environ-ments.In the present work,the tubular porous mullite supports werefabricated by the TBA-based freezing casting method,and theeffects of freezing temperatures,solid loadings and particle sizeon the porosity,pore size distribution,and subsequently onmechanical strength of the tubular porous mullite supports wereinvestigated.0955-2219/$–see front matter©2013Elsevier Ltd.All rights reserved. /10.1016/j.jeurceramsoc.2013.06.0053250R.Liu et al./Journal of the European Ceramic Society33(2013)3249–3256Fig.1.Schematic illustration of the container used in TBA-based freezing cast-ing.2.Experiment procedure2.1.Sample preparationCommercially available mullite powder(Songyan furnace powders Co.Ltd.,Henan,China)was used as the starting mate-rial.This mullite powder has a median size(d50)of14.7␮m and a specific surface area of1.24m2/g.Tert-butyl alcohol(TBA, chemical purity,Beijing Yili Chemical Co.,Beijing,China)and polyvinyl butyral(PVB)were used as the shaping vehicle and the binder in the freeze casting process,respectively.Fig.1illus-trates the container design for freezing TBA-based slurry.The container consists of a copper cylinder with high thermal con-ductivity,and Teflon rod andfloor with low thermal conductivity. The Teflon rod was placed in the center of the metal cylinder. The container was put into the cooling bath,which was adjusted to designed temperature(−20to100◦C).TBA ice stimulated to grow in the radial direction from the inner surface of the metal cylinder to its center region where the Teflon rod was placed.A premixed solution was prepared by mixing0.5wt%PVB into TBA.Mullite powder(20–40vol.%)was mixed with the premixed solution(60–80vol.%)and ball-milled for4h to gen-erate a homogeneous suspension.To adjust the suspension to a properflowability during casting,a selected small amount of dispersant(BYK163,5wt%,based on the weight of TBA)was added into the slurry.The slurry was de-aired by stirring under vacuum and then poured into the mold,finally subjected to uni-directionally freezing.After freezing,the frozen bodies were freeze-dried for12h in vacuum at−50◦C using a freeze-dryer (Type FD-1A-50,Boyikang Corp.,Beijing,China).Tubular green compacts with outer diameter of50mm,inner diameter of30mm and length of80mm were then prepared and carefully removed from the molds.Subsequently,the green compacts were sintered at1550◦C for2h in air.2.2.CharacterizationThe particle size distribution of commercial mullite powder was examined on a Mastersizer-2000laser particle analyzer. The microstructures of the sintered tubular porous mulliteTemperature (ºC)TG(%)DSC (mW/mg)Fig.2.TG-DSC curves of the green tubular porous mullite.supports were observed using scanning electron microscopy (SEM,JEOL JSM-7001F,Japan)after sputtering gold coating on the surfaces.In particular,in order to observe the pore channel size and microstructure of the section perpendicular to the freezing direction,the samples were infiltrated with epoxy resin to avoid breaking and make it more adaptive to the working condition.The porosity of the samples was evaluated by Archimedes method with a theoretical density of3.16g/cm3 for dense mullite.The average pore size and pore size dis-tribution were measured by a mercury intrusion porosimetry (AutoPore IV9510).The specific surface area was measured by a SI-MP-type specific surface area and porosity analyzer (Quantachrome Instruments,USA).The compressive strength was measured using cubic samples(10mm×10mm×10mm) (CSS-2220test machine,Changchun Research Institute for Mechanical Science Co.,Ltd.,China)along the radius direction. Four samples were used to determine the average compressive strength.The permeability of the supports was characterized by nitrogenflux and pure waterflux.The nitrogenflux of the supports was measured on home-made bubble-point apparatus with nitrogen as the permeation medium.The pure water flux of the supports was measured using cross-flowfiltration equipment under various pressures at ambient temperature.3.Results and discussion3.1.Thermal analysis of the green tubesThe TG-DSC analysis was used to evaluate the sintering behaviors of the green tubes after sublimation and drying pro-cess,and the results are showed in Fig.2.It can be seen that the weight loss of the green tubes in the sintering process can be divided into three stages.In thefirst stage,the weight loss was2.1%when the temperature elevates from the ambient tem-perature to367◦C,due to the volatilization of the residual TBA and H2O;the weight loss due to the volatilization of PVB was 1.1%when the temperature elevates from367◦C to600◦C;and after600◦C,the weight of the green tubes maintains the same, indicating the complete removal of the organic binder.It canR.Liu et al./Journal of the European Ceramic Society 33(2013)3249–32563251L o g D i f f e r e n t i a l I n s t r u s i o n (m L /g )m)Fig.3.Pore size distribution of porous mullite tubes with different solids loading.be deduced that the heating rate must be carefully controlled between 0to 367◦C and 367◦C to 600◦C in order to inhibit cracking of the porous mullite tubes during sintering process.3.2.Effect of solids loadingIn order to investigate the effects of solids loading on the microstructure and properties of the prepared tubular porous mullite supports,the freezing temperature and freezing time were fixed to −100◦C and 1h,respectively.Fig.3shows the pore size distribution of tubular porous mullite supports with different solids loading.It can be clearly seen that each case presented a bimodal pore size distribution with peak locations at 2.8–3.5␮m and 7.1–13.9␮m,respectively.One peak had a fixed pore size of 2.8–3.5␮m at all solids loading.These pores were resulted from both burn-out of binders and grain packing in the ceramic walls.The other peak was located in the range of relatively larger sizes of 7.1–13.9␮m.These pores are the dominated ones indicated from the relative height of the peak and they represented the unidirectionally aligned pore channels.With increasing solids loading,the size of larger pores towards to the lower direction,and it can be noted that the peak height of the larger pores decreases while smaller pores increases when the solid loading of the mullite powders are up to 40vol%.It can be attributed to the particle expulsion and hindrance effect.The rejection of solid particles at the solidification fronts is so effective that pore channels appear in the sample during freeze casting when the solids loading is relatively low,with the increas-ing of solids loading,the walls of pore channels become thicker and meanwhile,the pore channel size decreases.However,for higher solids loading samples (40vol.%),the rejection of solid particles is hindered by the crowded particles and the formation of pore channel is inhibited,and furthermore,additional solid particles also provide numerous heterogeneous nucleation sites for freezing of TBA,finally results homogeneous pore structure.Fig.4shows the porosity and mechanical strength variation of tubular porous mullite supports with different solidsloading.Solid loading (vol%)P o r o s i t y (%)Compressive strength (MPa)pressive strength and porosity of porous mullite tubes with different solids loading.It is found that with increases of the solids loading,the porosity of tubular porous mullite supports decreases,while the compres-sive strength increases.The porosity and compressive strength of tubular porous mullite supports ranges from 76.83%to 56.92%and 23.34MPa to 48.76MPa respectively when the solids load-ing increases from 20vol.%to 40vol.%.Higher solids loading suspensions possess lower TBA content and thus produce lower porosity and higher density of the freeze cast samples.3.3.Effect of freezing temperatureIn order to investigate the effects of freezing temperature on the microstructure and properties of the prepared tubular porous mullite supports,the solids loading and freezing time were fixed to 35vol.%and 1h,respectively.Fig.5shows the pore size distribution of the prepared tubular porous mullite supports with different freezing temperature.Likewise,each case presented a bimodal pore size distribution with peak loca-tions at 2.9␮m and 10.1–18.2␮m,respectively.One peak had a fixed pore size of 2.9␮m at all conditions.These poreswereFig.5.Pore size distribution of tubular porous mullite supports with different freezing temperature.3252R.Liu et al./Journal of the European Ceramic Society 33(2013)3249–3256Freezing temperature (C)P o r o s i t y (%)Compressive strength (MPa)pressive strength and porosity of porous tubes with different freezing temperature.resulted from both burn-out of binders and grain packing in the ceramic walls.The other peak was located in the range of relatively larger sizes of 10.1–18.2␮m.These pores are the uni-directionally aligned pore channels.With decreasing freezing temperature,the size of larger pores decreases,while the size of smaller pores remains intact.Freezing temperature affects the relative dominance of TBA ice nucleation and crystal growth.Under high supercooling,namely,lower freezing temperature,nucleation rate is higher than the crystal growth rate,so TBA ice nucleation is more favorable than crystal growth.At such freezing temperatures,a large number of small TBA ice crystals form.In contrast,if the freezing temperature is higher (super-cooling is low),a small number of large TBA ice crystals form during freeze casting,and the larger pores form after the ice sublimation.Fig.6shows the porosity and mechanical strength variation of tubular porous mullite supports with different freezing tem-perature.It can be found that,unlike the obvious effect on pore size,the effect of freezing temperature on total porosity is not obvious because of the fixed solid loading.With the rise of the freezing temperature,the porosity of tubular porous mullite sup-ports decreases slightly,just from 58.11%to 61.29%when thefreezing temperature reduces from −20◦C to −100◦C.The dis-persing state of the suspension is more likely to be maintained at a high freezing rate since there is less time for mullite particles to rearrange,and higher freezing temperature (lower freezing rate)provides particles with more time to rearrange,and thus the parti-cle packing is denser.Therefore,the lower freezing temperature produces a relative higher porosity in materials.The compressive strength of the tubular porous mullite sup-ports rapid decreases firstly,and then increases slightly with the rising of freezing temperature.It is due to the change of the uni-directional pore structure at a higher freezing temperature to the uniform pore structure at a lower freezing temperature.At rela-tively high freezing temperature,the growth of TBA ice results the small amounts of unidirectional pore channels with thicker walls,and with the decreases of the freezing temperature,the pore channel size decreases and the quantity of pore channels with thinner walls increases,leading to the decreasing of the compressive strength.However,TBA ice nucleation is kinet-ically more favorable than crystal growth,and uniform small pore formation is more likely when further decreasing the freez-ing temperature,and thus the compressive strength increases rapidly.3.4.Effect of particle size distribution of mullite powderTo obtain the powders with different particle size distribution,the as-received mullite powders were wet-milled by zirconia balls using distilled water as a liquid medium.Fig.7shows the effect of ball-milling time on the particle size distributions and average particle diameters of the mullite powders.The start-ing mullite powder exhibits an average particle diameter of 14.7␮m and a rather wide particle size distribution.A rela-tively large quantity of coarse particles (24.85%)shows a larger diameter than 30␮m.As a result of ball-milling of the initial powders,the change of its particle size distribution occurred.With the increasing ball-milling time,the particle size distri-butions become narrower gradually,especially for the powders after ball-milling for more than 24h.At the same time,particle diameter is fastly decreased with ball-milling time between 0and 24h,but then slightly decreased between 24h and 48h.The0.111010010000123456V o l u m e p e r c e n t (%)0122436482468A v e r a g e p a r t i c l e d i a m e t e r m )Ball-milling time (h)Fig.7.Effect of ball-milling time on the particle size distributions (a)and average particle diameters (b)of the industrial mullite powders.R.Liu et al./Journal of the European Ceramic Society 33(2013)3249–32563253L o g D i f f e r e n t i a l I n s t r u s i o n (m L /g )Cumulative pore volume (mL/g)Pore size diameter (m)L o g D i f f e r e n t i a l I n s t r u s i o n (m L /g )Cumulative pore volume (mL/g)Fig.8.Pore size distribution and cumulative pore volume of porous mullite supports with powder-C (a)and powder-B (b).average particle diameters are 14.7,6.5,3.8,3.2and 2.8␮m for 0,12,24,36and 48h respectively.Under the influence of capillary force,mullite particles entered the gaps between every two zirconia balls.The structural refinement was induced by the succession of impacts between the milling bodies,which determined the cold-welding and fracture of the powder particles trapped between the colliding surfaces.As a result,the powders were ground by shearing force when zirconia balls were rotated at a high speed.Most of the large particles were broken up because of the shearing force function,as well as the low bonding strength of industrial mullite solids themselves.In order to investigate the effects of particle size distribution on the characteristics of the tubular porous mullite supports,the powder-A (unmilled,mean particle size 14.7␮m),powder-B (ball-milling for 12h,mean particle size 6.5␮m)and powder-C (ball-milling for 48h,mean particle size 2.8␮m)were used to prepare tubular porous mullite supports when the solids loading was 35vol.%,freezing temperature was −100◦C and freezing time was 1h.Fig.8presents the pore size distribution of the porous mullite supports fabricated by milled mullite powders.Likewise,each case presented a bimodal pore size distribution with a narrower peak locations at 6.5–7.2␮m and wider peak locations at around 2.1␮m,respectively,and the smaller pores are formed by the particle accumulations,while the larger pores are formed by the sublimation of TBA ice.The pore channel size increases with the increases of average particle size of mullite powders.With increases of the milling time,both the size of the larger pores and smaller pores decreases.It is due to the decrease of the particle size distribution of mullite powders with increases of the milling time,for smaller pores,the size of pores formed by accumulations of mullite powders with smaller particle size is less and the pore size distributions are narrower than that of pores formed by accumulations of mullite powders with larger particle size.For lager pores,the smaller particle size not only provides more nucleation sites of TBA ice and results in the formation of small pores,but also reduces the mobility of the particles and results in the formation of more homogeneous pore structures,indicated by the cumulative pore volume curves in Fig.8.Fig.9shows the variation of porosity and compressive strength of the porous mullite supports with different particlesize.With increases of the particle size,the porosity increases slightly,while the compressive strength decreases,and it may be ascribed to the change of pore structure from homogeneous to unidirectional.It can be concluded that the microstructure and properties can be affected by the fabrication parameters of freezing casting,and the influencing factors are solids loading,freezing temperature and particle size of starting materials in order.3.5.Characteristics of the tubular porous mullite supports at different locationsIn order to characterization of the gradient pore structures of the tubular porous mullite supports,the tubes prepared with the average particle size of 2.8␮m of mullite powders,freez-ing temperature of −100◦C and solids loading of 35vol%were selected.Fig.10shows the photographs of the sintered tubular porous mullite supports.It can be found that the tubes are intact with smooth surfaces,and the pores are radially distributed.Fig.11shows the typical microstructure of the porous mul-lite supports fabricated by freeze casting.The architectures in the sintered samples were observed along the parallel direc-tions and perpendicular directions to the freezing direction,as shown in Fig.11(a)–(c)and (d)–(e),respectively.The paral-lel section to the freezing direction clearly indicated thatthe50607080m)P o r o s i t y (%)Compressive strength (MPa)pressive strength and porosity of tubes with different particle size distribution.3254R.Liu et al./Journal of the European Ceramic Society 33(2013)3249–3256Fig.10.Photographs of the sintered tubular porous mullite supports (a)and cross-section image(b).Fig.11.Typical SEM micrograph at different locations of porous mullite supports.(a)The outer surface of the tubes,(b)the center of the tubes,(c)the inner surface of the tubes,(d)perpendicular section to freezing direction (prepared by epoxy resin infiltration),and (e)perpendicular section to freezing direction.well-ordered micro-channeled structures is formed after freez-ing process (Fig.11(b)–(c)).And it also can be noted that with the increases of the distance away from the outer surface,the pore structure changes from homogeneous pores (Fig.11(a))to unidi-rectionally aligned pores (Fig.11(b)–(c)),and the pore channels tend to align with increasing pore channel size in the freezing direction.It is owing to the thermal resistance of the solidified layer,the solidification velocity decreased with increasing dis-tance and caused an increase of TBA prism spacing and thus pore channel size.Moreover,the perpendicular section to the freez-ing direction indicated that the ceramic walls were regularly arranged between the adjacent pore channels which showed a hexagonal cross section (Fig.11(d)and (e)).High-magnification image showed sub-micrometer sized pores on the pore walls (Fig.11(e)).Figs.12and 13illustrate the variation of pore size distribution and cumulative pore areas at different locations of tubular porous mullite supports respectively.The pore channel size and pore area increases with distance away from the outer surface.TheL o g D i f f e r e n t i a l I n s t r u s i o n (m L /g )m)Fig.12.Pore size distribution at different locations of tubular porous mullite supports.(a)Outer surface,(b)the center of the tubes,and (c)inner surface.R.Liu et al./Journal of the European Ceramic Society 33(2013)3249–325632550.00.10.20.30.40.50.6C u m u l a t i v e p o r e a r e a (m 2/g )Pore diameter (nm)Fig.13.Cumulative pore area at different locations of tubular porous mullite supports.pore channel sizeincreases from 7.2␮m near the outer surface to 9.1␮m near the inner surface of the tube,which is consis-tent with the SEM observations.The pore area near the outer surface of the tubular porous mullite supports was 0.47m 2/g,while the pore area of the center and inner locations of the tube was 0.51m 2/g and 0.55m 2/g,respectively.The test results of specific surface area also shows the same rules,and the spe-cific surface area of the outer surface,center,and inner surface of tubes was 0.78m 2/g,0.87m 2/g and 1.02m 2/g,respectively.The above results indicated that the tubular porous mullite sup-ports prepared by TBA-based freezing casting method possesses a gradient pore structure with unidirectionally aligned pores,and it will be favorable for the separation process.Fig.14presents the nitrogen flux and pure water flux of the supports at different pressures.It can be seen that the nitrogen flux and pure water flux increases with increases of the pressure,and the nitrogen flux and pure water flux at different pressures are all higher than the supports reported before.5,9,25,26When a gas flow in porous supports dominated by the viscous flow regime,gas flux is proportional to open porosity and the square of pore size according to the Hagen-Poiseuille equation,27and the poreAverage pressure (MPa)N i t r o g e n f l u x 102m 3/m h )Pure water flux (m 3/m Fig.14.The nitrogen flux and pure water flux of the supports under various pressures.size also has a stronger impact on pure water flux than porosity.26The unidirectionally aligned pores with gradient distribution of the supports may beneficial for the improvement of the flux.4.ConclusionsThe tubular porous mullite supports were successfully fabri-cated by the TBA-based freezing casting method with different solids loading,freezing temperature and starting particle size.The unidirectionally aligned pore structures with gradient dis-tribution along the freezing direction were obtained,which is potential for the applications in ceramic membrane supports and micro-filtration of ceramic membranes.The microstructures and properties of the tubular porous mullite supports can be effectively adjusted by controlling the freezing temperature,sus-pension solids loading and particle size.The pore channel size decreased significantly with increasing suspension solids load-ing,decreasing freezing temperature and reducing the particle size.The porosity also decreases with increases of solids load-ing and freezing temperature,as well as reduces of the particle size,while the compressive strength increases.Summary of novel conclusionsPorous tubular mullite supports with gradient unidirectional aligned pores were successfully fabricated by TBA-based freez-ing casting method.The effects of freezing temperature,solids loading in the suspension and particle size distribution of mullite powders on the microstructure and properties of the tubular porous mullite supports were investigated extensively.The results show that the pore size,porosity and compressive strength of the tubular porous mullite supports can be effectively adjusted by controlling the freezing temperature,solids loading and particle bined with the results of microstructure observations,pore size distribution and specific surface area,it indicates that the pore channel size increases along the freezing direction,accompanied by the changes of pore structure from homogeneous near the freezing medium to unidirectional away from the freezing medium.The pore channel size decreases sig-nificantly with increasing solids loading,decreasing freezing temperature and reducing the particle size.The porosity also decreases with increases of solids loading and freezing tempera-ture,as well as reduces of the particle size,while the compressive strength increases.The tubular porous mullite supports with 6.5of pore channel size,59.66%of porosity and 54.11MPa of com-pressive strength were obtained when the freezing temperature,solids loading and average particle size was -100◦C,35vol%and 2.8␮m,respectively.AcknowledgmentsThe authors would like to thank the financial support from the National Natural Science Foundation of China (NSFC-No.51172119and 51202117).3256R.Liu et al./Journal of the European Ceramic Society33(2013)3249–3256References1Hua FL,Tsang YF,Wang YJ,Chan SY,Chua H,Sin SN.Performance study of ceramic microfiltration membrane for oily wastewater treatment.Chem Eng J2007;128:169–75.2Cerneaux S,Stru˙z y´n ska I,Kujawski WM,Persin M,Larbot A.Comparison of various membrane distillation methods for desalina-tion using 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牵引车-飞机系统的路径跟踪控制(英文)

牵引车-飞机系统的路径跟踪控制(英文)

J.Marine Sci.Appl.(2012)11:512-517DOI:10.1007/s11804-012-1162-xPath-tracking Control of a Tractor-aircraft SystemNengjian Wang,Hongbo Liu*and Wanhui YangSchool of Mechanica l and Electr ical Engineering,Har bin Engineering Univer sity,Ha rbin150001,ChinaAbstra ct:An aircraft tractor plays a significant role as a kind of important marine transport and supportequipment.It’s necessary to study its controlling and manoeuvring stability to improve operation efficiency.Avirtual prototyping model of the tractor-aircraft system based on Lagrange's equation of the first kind withLagrange mutipliers was established in this paper.According to the towing characteristics,a path-trackingcontroller using fuzzy logic theory was designed.Direction control herein was carried out through acompensatory tracking approach.Interactive co-simulation was performed to validate the path-trackingbehavior in closed-loop.Simulation results indicated that the tractor followed the reference courses preciselyon a flat ground.Keywords:path-tracking controller;aircraft tractor;preconcert route;fuzzy control;co-simulationArticle ID:1671-9433(2012)04-0512-061Introduction1Automatic guidance of industrial articulated vehicles,such as mining trucks,earth-removal and road-paving vehicles, intercity bus travels,and automated guided vehicles(AGVs), (Lane et al.,1994;Larsson et al.,1994;Hirose et al.,1995; Rabinovitch and.Leitman,1996;de Santis,1997;Lamiraux et al.,1999);have over80years,received a great deal of attention from researchers.Recently,a study in intelligent control technology for maritime applications has prompted more research investigating.For more than20years the study of tractor aircraft systems has provided vital information for on researching maritime vessel transportation.The process has been noted as to being a complicated nonholonomic, under-actuated and nonlinear system.The path-tracking plays a significant role in improving operation efficiency(Rifford, 2004,2006,2008;Nakamura et al.,2001).Wang(1994) Aircraft tractors are essential tools for aircraft movement on large ships,as well as takeoff and landing.The mechanism is different from a shore-based allocation and transporting of an aircrafts;tractors on the ship are placed in less than ideal environments,narrow space and exclusive transportation facilities by Han et al.(2010).Relatively good transport efficiency and flexibility are required during these tasks.As a result,the lack of maneuverability has increased a higher rate of involvement in fatal accidents.Through constant evolution and development of computer and sensor technologies,research on tracking control methods for two-wheeled and car-like mobile robots have increased significantly(de Wit et al.,1993;Kanayama et al.,1990,1991; Murray and Sastry,1993;Samson and Ait-Abderrahim,1991a, Received d at e:2011-11-13.Found at ion item:Harbin Technological Innovation ResearchFund(NO:2012RFXXG039)*C orresp ond ing aut hor Email:lhbci************©Harbin Engineering Univers ity and Springer-Verlag Berlin Heidel berg20121991b).In addition,a few researchers have explored in greater detail the study of tracking control of trailer systems,which basically consist of a steering tractor and a passive trailer, linked with a rigid joint,such as a tractor-aircraft system.As noted in the references listed:(Lamiraux and Laumond,1997; Sekhavat et al.,1997;Yuan and Huang,2006)much of the interest driving experimentation,is the utilization of trailers on mobile robots.However,problems occur due to the controlling of the system from the viewpoint of the mobile robot and not a passive trailer.In1994,de Santis,conducted a simple linear control study using a linearized model designed for a trailer system.The research is of great interest and a positive perspective on the study of tracking control systems guide points have been explored for future recommendations.The study was divided into three components:First, analyzing the tractor aircraft systems,examining the marine transport equipment,and understanding the procedures of the maneuvering stability of a ship.Next,the research focused on guiding a path tracking controlled aircraft tractor into preconcerted routes and keeping a smooth motion, almost like a flat ground on a ship.Thirdly,the paper focused on analyzing the performance of the tractor in an automatic navigation system setting.The research study utilized the fuzzy logic theory as a measuring tool in the designing of the controller for the tractor-aircraft system.The researcher also took into account factors for the adverse ef fects,caused by factors such as tire slippage.The direction control was performed through a compensatory tracking approach method.The organizational flow of the research paper has been divided into five sections.In section II,the research focused on the kinematic and virtual prototyping model of the aircraft-tractor system.Section III,focused on theJournal of Marine S cience and Appl ication (2012)11:512-517513design of the fuzzy control system,while section IV contains simulation results.The paper concludes with remarks and recommendations in section V .2Model of a tr actor-aircraft system2.1Kinematic mod elThe model is based on a rigid multiply body that consists of a tractor,a drawbar,the undercarriage and fuselage,ignoring,for the moment,the flexibility of the tractor suspension and undercarriage buffer system.It is usually assumed that the wheels do not slip.The deformation of the tires is also ignored for the sake of simplicity.These assumptions are acceptable for tractor towing at low speeds:(1)Calculate the lateral component of constraint force onthe tractor-aircraft system junction.(2)The relative angles between the various parts are small,and the tractor front wheel steering angle is small.(3)Examine the wheels rolling resistance,back torque and air resistance.Primarily consider the lateral and the swaying motions of the tractor-aircraft system illustrated in Figure1.Fig.1Kinematic model of a tractor-aircraft system Dynamical equations of the tractor are shown as the following.11111121()cosy a y y m v u r F F F R (1)111122131cos z y y y a J r F d F d R d M (2)The drawbar and the nose landing gear dynamical equations are depicted as:2222323()y y y m v u r R R F (3)22243535z y y y J r R d R d F d (4)Dynamical equations of the fuselage and the rear landinggear are founded with the expression3333244()a y y m v u r F F R (5)3346247z y a y J r R d M F d (6)where i m represents the mass (the subscript i=1,2,3denotes the tractor,the drawbar and the aircraft respectively),i u is the marching velocity,i r is the sway rate and yi F is the cornering force on the tractor wheel,yi R is the lateral constraint reacting force on the articulation and the vertical moment of inertia is expressed with iz J ,ai F and ai M are the accessional lateral force and torque on the centroid,δis the tractor front wheel steering angles,12,d d are the distances from the tractor centroid to the front and rear axle,3d is the distance from the tractor centroid to the anterior to the drawbar,45,d d are the distances from the drawbar centroid to its foreside and rearward,67,d d are thedistances from the aircraft centroid to the front and rear axle.Cornering force on the tractor wheels yi F is defined as a function of the slip angle.When the lateral acceleration is less than 0.4g,the slip angle is generally no more than 4°-5°,the tire cornering properties are in the linear range.Cornering force is given by y i i i F k a ,where i k is thecornering stiffness,its value is negative,i a is the tire slipangle.The state equation of tractor-aircraft towing operation can be described by means of:K XL XM UN TS F(7)2.2Vir tual prototyping modelUsing the ADAMS/View program(Elliott,2000),a virtual prototyping model is created as shown in Figure 2.A centralized quality tractor model is established,which includes the body,suspension and steering system,tires and other components.The study shows evidence of a reduction in the drawbar to a cylindrical rod..The aircraft model is mainly composed of the fuselage,undercarriage and employs spring-dampers.As a result,nonlinear elastic damping effects in the spline curve takes place in the undercarriage buffer system.Nengjian W ang,et al.Path-tracking C ontrol of a T ract or-A ircraft System514Fig.2Virtual prototyping model of the tractor-aircraftsystemThe parameters of the tire and road can be set in the Fiala tyre model and mdi_2d_flat road model,such as:the vertical stiffness,vertical damping of the tire,the friction factor ,and graphics of the road.2.3Comparative analysis of kinetic model an d virtualprototype mod elA comparative analysis was conducted to set the tractor initial position on the ground coordinate system origin and zero degree for the initial direction.The simulation was carried out using a vertical speed of 5km/h.The step input was given to a steering wheel with the function:step (time,8,0,8.02,and 42d).The study compared the steady-state values of the kinetic model and the virtual prototype model,as shown in Table 1.It was established that the virtual prototype model is a good feature.Table 1Contrast of the Kinetics ParametersInvestigating variablesY aw rate of the tractor/((°)·s 1)Yaw rate of thedrawbar/((°)·s 1)Y aw rate of the aircraft/((°)·s 1)Lateral velocityof the tractor/(mm/s)Angle between the drawbar and the aircraft/(°)Angle betweenthe tractor and the drawbar/(°)Simulation value1.4361.4271.40445.904.1266.222Theoretic value 1.507 1.507 1.47846.60 4.395 6.549Absolute error 0.0740.0800.0740.7000.2690.327Relative error5.3%5.6%5.3%1.5%6.5%5.2%3Establishment of fuzzy control sysytemBased on the virtual prototype model of the tractor-aircraftsystem a Mamdani fuzzy control system is established (Shukla and Tiwari,2010).A block diagram of the fuzzy control system is visible in Figure 3.Distance deviation and angle deviation,which can be derived by drawing acomparison between the actual path,and the preconcerted routes are calculated as the input of the controller.The torque that controls the steering wheel angle sheers off betimes to eliminate the error is referred to as the output.Fig.3Block diagram of the controller3.1Path Reference fr ameUbiety between the tractor and the preconcerted route is shown in Figure4.The ground coordinate system OX YZ is used to describe the trajectory,whereas vehicle coordinated system oxyz is used to calculate the distance deviation Ed and angle deviation Ea.Path point P c (c=1,2,3,…n)connecting to the sequentially composed preconcerted path.The origin of the vehicle system of coordinates is (X 0,Z 0)on the ground coordinate and the relative angle between these two coordinated systems is .Fig.4Schematic diagram of the ubiety3.2Posit ion ControllerJournal of Marine S cience and Appl ication (2012)11:512-517515The functions of the fuzzification interface are to perform the following steps:measure the values among the input variables from the data acquisition interface,quantifying in order to transform the range of the observed values into the corresponding discourse of the language variables,and transforming the input data into proper linguistic values,that can be regarded as a form of fuzzy set.The subets of the in-out variables are decomposed into seven fuzzy partitions,denoted by PB (positive big),PM (positive medium),PS (positive small),Z (zero),NS (negative small),NM (negative medium),and NB (negative big),respectively.The domain of distance deviation,Ed is [–1000,1000],Unit:mm and of angle deviation Ea is [1.57,1.57],Unit:rad.Control axial torque on the steering wheel has a basic domain of [78400,78400]which unit is N ·mm.In-out variables in fuzzy set are on the fuzzy domain {6,4,2,0,2,4,6}.Analyzing the basic domain and the compartmentalization of the hierarchy,quantization factor of distance deviation Kd comes to a value of 0.006and that of angle deviation Ka is 0.267,while the control torque scale factor Kt is 13066.The membership function of in-out is shown in Figure5.Fig.5Membership functionThe rule table of fuzzy controller is shown in Table 2and the output surface of fuzzy control rules can be illustrated as shown in Figure6.There are four conditions of the tractor current position and preconcerted route determined by the distance and angle deviation:(a)0,0Ed Ea ;(b)0,0Ed Ea ;(c)0,0EdEa;(d)0,0EdEaTable 2Rule table of fuzzy controllerOutput Torque UEd NB NM NS Z PS PM PB Ed NB PB PB PB PM NS NS NS NM PB PB PM PS NS NS NS NS PB PM PM PS NS NS NS ZPM PM PM Z NM NM NM PS PS PS PS NS NM NM NB PM PS PS PS NS NM NB NB PBPSPSPSNMNBNBNBEd EaFig.6Output surface of fuzzy rules4Tracking behavior simulation analysisFor verifying the efficiency of the proposed controller,we realize this system on the virtual prototyping model created in section Ⅱ.Define the in-out adopting ADAMS/Controls and establish the control algorithms in Simulink Model.The study implemented control modules and designed software in the control system,and interactive simulation.The co-simulation model is shown in Figure7,which contains dynamic modules;path deviation calculation module,a fuzzy control module and a time limit module.The corresponding oscilloscope to record the distance and angle deviation and other important data were also established.Thus,the operations and some experimental results are presented in a series of pictures to demonstrate the efficiency of the proposedmethods.Fig.7Co-simulation mode l4.1Performance of the Virtu al Prototyping ModelGiven the tractor rear wheel,a axial torque with a step input:step (time,0,50000,180,1800000)and a drive function to the steering wheel with:step (time,0,0,1,168d),the simulation was carried out.The traction trajectory is shown in Figure 8.The simulations illustrated in Figs.7and 8,results indicate that the under-steer system increased the tractor turningNengjian W ang,et al.Path-tracking Control of a T ractor-A ircraft System 516radius and lateral velocity.t.The tractor's turning radius andlateral velocity are greater than those of the aircraft.Aforesaid analysis proves that the virtual prototyping modelhas good maneuveringstability.(a)Route of the Idle Load Tractor(b)Route of the Load-CarryingTractor(c)Route of the Passive AircraftFig.8TractionTrajectoryFig.9Turning Radius of theTractorFig.10Lateral Velocity Comparison4.2Tr acking Beh avior Und er th e Fuzzy Con trolTowing the aircraft at the speed of5.4km/h along route1(visible in Fig.11),simulations was carried out as follows:(a)Running with a step input:step(time,4,0,4.2,42d)(b)Control the system through co-simulation approachWe investigate the performance of the fuzzy control system.Figure12shows the tracking behavior under an operation ofclosed-loop input.The foundation of the fuzzy controllercould make up some adverse effects caused by tire slippage,etc,to a certain extent.Also the establishment plays animportant role in safe and efficient towingoperation.Fig.11PreconcertedRoutesFig.12Tracking TrajectoriesThe tractor drove in accordance with the intended route2asshown in Figure13,pulling the aircraft from point A todestination B at the speed of 5.4km/h.The trackingtrajectories also obtained the kinetics parameters during thetask from the co-simulation.Figure12shows the lateralvelocity and turn angle of the aircraft for wheel values.Themaximum kinetics parameters are also shown in Tab.4characterizing the towing performance.Therefore,using the designed controller to guide thetraction system tracking in an intended route under practicaltraction work conditions issafe.(a)L ateral Velocity of theTractor(b)Turn Angle of the Aircraft Fore-wheelFig.13Kinetics ParametersJournal of Marine S cience and Appl ication(2012)11:512-5175175ConclusionsFor the automatic guidance and stability control of the ship-based tractor-aircraft system,a fuzzy control system was designed.Firstly,taking into account lateral and the swaying motions,a nonlinear dynamic model is introduced.A virtual prototyping model,which has good maneuvering stability,is established.Furthermore,based on the fuzzy logic,the controller is derived based on the virtual prototyping model.The simulation results confirm the fuzzy control system effectively enables the traction system to track the preconcerted path well.Under the control of the designed controller,the tractor-aircraft system provided a good description of the dynamic behavior.ReferencesDe Santis RM(1994).Path-tracking for a tractor-trailer-like robot.Int J Robot Res,13(6),533-543.De Santis R(1997).Modeling and path-tracking for a load-haul-dump vehicle.J.Dynam.Sy st.Mea s.Contr.,119, 40-47.De Wit C,Khennouf H,Samson C,Sordalen OJ(1993).Nonlinear control design for mobile robots,recent trends in mobile robots.World Scientific Series in Robotics and A utomated Systems,11, 121-156.Elliott AS(2000).A highly efficient,general purpose approach for cosimulation with ADAMS.MDI North A mer,User Conf.,MI,. Han F,Yang BH,Wang HD,Bi YQ(2010).The optimizing research on aircraft handling workflow.Science Technologya nd Engineer ing,10(22),5602-04.Hirose S.Fukushima E,Tsukagoshi S(1995).Basic steering control methods for the articulated body mobile robot.IEEE Contr.Syst.Mag.,4,5-14.Kanayama Y,Kimura Y,Miyazaki F,Noguchi T(1990).A stable tracking control method for an autonomous mobile robot.IEEE Int Conf on Robotics and A utomation,Cincinnati,OH, 384-389.Kanayama Y,Kimura Y,Miyazaki F,Noguchi T(1991).A stable tracking control method for a non-holonomic mobile robot.Int Conf on Intelligent Robotics Systems,Osaka,Japan,1236-1241. Lamiraux F,Laumond JP(1997).A practical approach to feedback control for a mobile robot with trailer.IEEE Int Conf on Robotics a nd A utoma tion,leuv en,Belgium,3306-3311. Lamiraux F,Sekhavat S,Laumond J(1999).Motion planning and control for Hilare pulling a trailer.IEEE Tra ns.Robot.Automa t, 15,640-652.Lane J,King R(1994).Computer-assisted guidance of an underground mine truck.IEEE Int.Conf.Robotics a nd Automation,San Francisco,420-425.Larsson U,Zell C,Hyppa K,Wernesson A(1994).Navigating an articulated vehicle and reversing with a trailer.IEEE Int.Conf.Robotics a nd A utoma tion,San Francisco,2398-2404.Murray RM,Sastry S(1993).Nonholonomic motion planning: Steering using sinusoids.IEEE T r ans A utomat Contr,38(5), 700-716.Nakamura Y,Ezaki H,Tan Y,Chung W(2001).Design of steering mechanism and control of nonholonomic trailer systems.IEEE Transactions on Robotics and A utomation,17(3),367-374. Rabinovitch J,Leitman J(1996).Urban planning in Curitiba.Sci.A mer.,274(3),46-53.Rifford L(2008).Stabilization problem for nonholonomic control systems.Geometr ic Contr ol and N onsmooth A nalysis,Series on A dvances in Mathematics for A pplied Sciences,76,260-269.Rifford L(2006).The stabilization problem on surfaces.Control Theory a nd Stabilization II,64(1),55-61.Rifford L(2004).The stabilization problem:AGAS and SRS feedbacks.Optimal Control,Stabilization,and Nonsmooth Analysis.L ectures N otes in Control a nd Information Sciences, 301,173-184.Samson C,Ait-Abderrahim K(1991a).Feedback stabilization of a nonholonomic wheeled mobile Robot.Int Conf on Intelligent Robotics Systems,1242-1247.Samson C,Ait-Abderrahim K(1991b).Feedback control of a nonholonomic wheeled cart in cartesian space.IEEE Int Conf on Robotics and Automation,1136-1141.Sekhavat S,Lamiraux F,Laumond JP,Bauzil G,Ferrand A(1997).Motion planning and control for Hilare pulling a trailer.IEEE Int Conf on Robotics and A utomation,L euven,Belgium, 3306-3311.Shukla S,Tiwari M(2010).Fuzzy logic of speed and steering control system for three dimensional lines following of an autonomous vehicle.Inter national Journa l of Computer Science and Information Security,7(3),101-108.Wang Y(1994).Development of aircraft-towing tractor.Inter-national A viation,11(9),18-20.Yuan J,Huang YL(2006).Path following control for tractor-trailer mobile robots with two kinds of connection structures.IEEE/RSJ International Conference on Intelligent Robots and Systems,Beijing,China,2533-2538.Nengjian Wang was born in1962.He has been aprofessor at Harbi n Engineering University since2003.He has been a s upervisor for decades.Hisresearch covers a wide range of problems inmodern manufact uring systems theory,workshopand logistics scheduling and optimization,comput er-aided process planning and mechanicaldynamics.Hongbo Liu was born in1987.She is working ondoctoral degree at Harbin Engineering University.She mainly engages in computer simul ation,anal ysis of ai rcraft tracti on system dynamics andstabilit y control study.。

Adaptive cooperative tracking control of higher-order nonlinear systems with

Adaptive cooperative tracking control of higher-order nonlinear systems with
Automatica 48 (2012) 1432–1439
Contents lists available at SciVerse ScienceDirect
Automatica
journal homepage: /locate/automatica
Brief paper
Article history: Received 30 November 2010 Received in revised form 22 July 2011 Accepted 12 December 2011 Available online 8 June 2012 Keywords: Consensus Cooperative control Multi-agent system Neural adaptive control Nonlinear system Synchronization
✩ This work was supported by NSF grant ECCS-1128050, AFOSR grant FA9550-091-0278, and ARO grant W91NF-05-1-0314. The material in this paper was partially presented at the IEEE Conference on Decision and Control (CDC), December 15–17, 2010, Atlanta, Georgia, USA. This paper was recommended for publication in revised form by Associate Editor Shuzhi Sam Ge under the direction of Editor Miroslav Krstic. E-mail addresses: hwzhang@ (H. Zhang), lewis@ (F.L. Lewis). 1 Tel.: +1 817 272 5972; fax: +1 817 272 5989.

牛津译林版2020-2021学年九年级上册期末备考--知识点归纳(测试版)

牛津译林版2020-2021学年九年级上册期末备考--知识点归纳(测试版)

牛津译林版2020-2021学年九年级上册期末备考--知识点归纳Unit1一、impatient adj. 不耐烦的,急躁的【点拨】impatient是由“否定前缀im-+形容词patient”构成的形容词。

常用短语为…,意为“对……不耐烦”。

我们不应该对别人不耐烦。

【拓展】in-, im-, un-, dis-等都可用作否定前缀,放在一些形容词或动词前面表示否定。

correct正确的→incorrect不正确的;polite礼貌的→impolite没礼貌的,粗鲁的;necessary必要的→unnecessary 不必要的;agree同意→disagree不同意二、show off 炫耀,卖弄【点拨】show off 是动词和副词构成的短语,代词作其宾语时,必须放在show与off之间。

意为“向某人炫耀某物”。

她喜欢炫耀她的精美的服装。

【拓展】与show相关的短语:向某人展示某物带领某人参观某地三、pay attention to 注意【点拨】pay attention to中的to是介词,后跟名词、代词或v.-ing形式作宾语。

不要管我,请好好款待女客。

老师说:“请注意听。

”【拓展】与attention搭配的常用短语:注意某事引起某人的注意吸引某人的注意四、lead n. 领先地位;榜样【点拨】意为“处于领先地位”。

Our school soccer team has taken the lead by scoring a goal in the very first minute of the match.我们校足球队在比赛一开始就率先进球。

【拓展】(1)lead作名词,还有“主角”之意。

(2)lead作动词,意为“引导,带领”。

意为“导致”。

五、fall behind 落后【点拨】fall behind中的fall为系动词。

fall还可作实义动词,意为“落下,跌落”。

如果你不努力学习,就会落后于其他学生。

An Overview of Recent Progress in the Study of Distributed Multi-agent Coordination

An Overview of Recent Progress in the Study of Distributed Multi-agent Coordination

An Overview of Recent Progress in the Study of Distributed Multi-agent CoordinationYongcan Cao,Member,IEEE,Wenwu Yu,Member,IEEE,Wei Ren,Member,IEEE,and Guanrong Chen,Fellow,IEEEAbstract—This article reviews some main results and progress in distributed multi-agent coordination,focusing on papers pub-lished in major control systems and robotics journals since 2006.Distributed coordination of multiple vehicles,including unmanned aerial vehicles,unmanned ground vehicles and un-manned underwater vehicles,has been a very active research subject studied extensively by the systems and control community. The recent results in this area are categorized into several directions,such as consensus,formation control,optimization, and estimation.After the review,a short discussion section is included to summarize the existing research and to propose several promising research directions along with some open problems that are deemed important for further investigations.Index Terms—Distributed coordination,formation control,sen-sor networks,multi-agent systemI.I NTRODUCTIONC ONTROL theory and practice may date back to thebeginning of the last century when Wright Brothers attempted theirfirst testflight in1903.Since then,control theory has gradually gained popularity,receiving more and wider attention especially during the World War II when it was developed and applied tofire-control systems,missile nav-igation and guidance,as well as various electronic automation devices.In the past several decades,modern control theory was further advanced due to the booming of aerospace technology based on large-scale engineering systems.During the rapid and sustained development of the modern control theory,technology for controlling a single vehicle, albeit higher-dimensional and complex,has become relatively mature and has produced many effective tools such as PID control,adaptive control,nonlinear control,intelligent control, This work was supported by the National Science Foundation under CAREER Award ECCS-1213291,the National Natural Science Foundation of China under Grant No.61104145and61120106010,the Natural Science Foundation of Jiangsu Province of China under Grant No.BK2011581,the Research Fund for the Doctoral Program of Higher Education of China under Grant No.20110092120024,the Fundamental Research Funds for the Central Universities of China,and the Hong Kong RGC under GRF Grant CityU1114/11E.The work of Yongcan Cao was supported by a National Research Council Research Associateship Award at AFRL.Y.Cao is with the Control Science Center of Excellence,Air Force Research Laboratory,Wright-Patterson AFB,OH45433,USA.W.Yu is with the Department of Mathematics,Southeast University,Nanjing210096,China and also with the School of Electrical and Computer Engineering,RMIT University,Melbourne VIC3001,Australia.W.Ren is with the Department of Electrical Engineering,University of California,Riverside,CA92521,USA.G.Chen is with the Department of Electronic Engineering,City University of Hong Kong,Hong Kong SAR,China.Copyright(c)2009IEEE.Personal use of this material is permitted. However,permission to use this material for any other purposes must be obtained from the IEEE by sending a request to pubs-permissions@.and robust control methodologies.In the past two decades in particular,control of multiple vehicles has received increas-ing demands spurred by the fact that many benefits can be obtained when a single complicated vehicle is equivalently replaced by multiple yet simpler vehicles.In this endeavor, two approaches are commonly adopted for controlling multiple vehicles:a centralized approach and a distributed approach. The centralized approach is based on the assumption that a central station is available and powerful enough to control a whole group of vehicles.Essentially,the centralized ap-proach is a direct extension of the traditional single-vehicle-based control philosophy and strategy.On the contrary,the distributed approach does not require a central station for control,at the cost of becoming far more complex in structure and organization.Although both approaches are considered practical depending on the situations and conditions of the real applications,the distributed approach is believed more promising due to many inevitable physical constraints such as limited resources and energy,short wireless communication ranges,narrow bandwidths,and large sizes of vehicles to manage and control.Therefore,the focus of this overview is placed on the distributed approach.In distributed control of a group of autonomous vehicles,the main objective typically is to have the whole group of vehicles working in a cooperative fashion throughout a distributed pro-tocol.Here,cooperative refers to a close relationship among all vehicles in the group where information sharing plays a central role.The distributed approach has many advantages in achieving cooperative group performances,especially with low operational costs,less system requirements,high robustness, strong adaptivity,andflexible scalability,therefore has been widely recognized and appreciated.The study of distributed control of multiple vehicles was perhapsfirst motivated by the work in distributed comput-ing[1],management science[2],and statistical physics[3]. In the control systems society,some pioneering works are generally referred to[4],[5],where an asynchronous agree-ment problem was studied for distributed decision-making problems.Thereafter,some consensus algorithms were studied under various information-flow constraints[6]–[10].There are several journal special issues on the related topics published af-ter2006,including the IEEE Transactions on Control Systems Technology(vol.15,no.4,2007),Proceedings of the IEEE (vol.94,no.4,2007),ASME Journal of Dynamic Systems, Measurement,and Control(vol.129,no.5,2007),SIAM Journal of Control and Optimization(vol.48,no.1,2009),and International Journal of Robust and Nonlinear Control(vol.21,no.12,2011).In addition,there are some recent reviewsand progress reports given in the surveys[11]–[15]and thebooks[16]–[23],among others.This article reviews some main results and recent progressin distributed multi-agent coordination,published in majorcontrol systems and robotics journals since2006.Due to space limitations,we refer the readers to[24]for a more completeversion of the same overview.For results before2006,thereaders are referred to[11]–[14].Specifically,this article reviews the recent research resultsin the following directions,which are not independent but actually may have overlapping to some extent:1.Consensus and the like(synchronization,rendezvous).Consensus refers to the group behavior that all theagents asymptotically reach a certain common agreementthrough a local distributed protocol,with or without predefined common speed and orientation.2.Distributed formation and the like(flocking).Distributedformation refers to the group behavior that all the agents form a pre-designed geometrical configuration throughlocal interactions with or without a common reference.3.Distributed optimization.This refers to algorithmic devel-opments for the analysis and optimization of large-scaledistributed systems.4.Distributed estimation and control.This refers to dis-tributed control design based on local estimation aboutthe needed global information.The rest of this article is organized as follows.In Section II,basic notations of graph theory and stochastic matrices are introduced.Sections III,IV,V,and VI describe the recentresearch results and progress in consensus,formation control, optimization,and estimation.Finally,the article is concludedby a short section of discussions with future perspectives.II.P RELIMINARIESA.Graph TheoryFor a system of n connected agents,its network topology can be modeled as a directed graph denoted by G=(V,W),where V={v1,v2,···,v n}and W⊆V×V are,respectively, the set of agents and the set of edges which directionallyconnect the agents together.Specifically,the directed edgedenoted by an ordered pair(v i,v j)means that agent j can access the state information of agent i.Accordingly,agent i is a neighbor of agent j.A directed path is a sequence of directed edges in the form of(v1,v2),(v2,v3),···,with all v i∈V.A directed graph has a directed spanning tree if there exists at least one agent that has a directed path to every other agent.The union of a set of directed graphs with the same setof agents,{G i1,···,G im},is a directed graph with the sameset of agents and its set of edges is given by the union of the edge sets of all the directed graphs G ij,j=1,···,m.A complete directed graph is a directed graph in which each pair of distinct agents is bidirectionally connected by an edge,thus there is a directed path from any agent to any other agent in the network.Two matrices are used to represent the network topology: the adjacency matrix A=[a ij]∈R n×n with a ij>0if (v j,v i)∈W and a ij=0otherwise,and the Laplacian matrix L=[ℓij]∈R n×n withℓii= n j=1a ij andℓij=−a ij,i=j, which is generally asymmetric for directed graphs.B.Stochastic MatricesA nonnegative square matrix is called(row)stochastic matrix if its every row is summed up to one.The product of two stochastic matrices is still a stochastic matrix.A row stochastic matrix P∈R n×n is called indecomposable and aperiodic if lim k→∞P k=1y T for some y∈R n[25],where 1is a vector with all elements being1.III.C ONSENSUSConsider a group of n agents,each with single-integrator kinematics described by˙x i(t)=u i(t),i=1,···,n,(1) where x i(t)and u i(t)are,respectively,the state and the control input of the i th agent.A typical consensus control algorithm is designed asu i(t)=nj=1a ij(t)[x j(t)−x i(t)],(2)where a ij(t)is the(i,j)th entry of the corresponding ad-jacency matrix at time t.The main idea behind(2)is that each agent moves towards the weighted average of the states of its neighbors.Given the switching network pattern due to the continuous motions of the dynamic agents,coupling coefficients a ij(t)in(2),hence the graph topologies,are generally time-varying.It is shown in[9],[10]that consensus is achieved if the underlying directed graph has a directed spanning tree in some jointly fashion in terms of a union of its time-varying graph topologies.The idea behind consensus serves as a fundamental principle for the design of distributed multi-agent coordination algo-rithms.Therefore,investigating consensus has been a main research direction in the study of distributed multi-agent co-ordination.To bridge the gap between the study of consensus algorithms and many physical properties inherited in practical systems,it is necessary and meaningful to study consensus by considering many practical factors,such as actuation,control, communication,computation,and vehicle dynamics,which characterize some important features of practical systems.This is the main motivation to study consensus.In the following part of the section,an overview of the research progress in the study of consensus is given,regarding stochastic network topologies and dynamics,complex dynamical systems,delay effects,and quantization,mainly after2006.Several milestone results prior to2006can be found in[2],[4]–[6],[8]–[10], [26].A.Stochastic Network Topologies and DynamicsIn multi-agent systems,the network topology among all vehicles plays a crucial role in determining consensus.The objective here is to explicitly identify necessary and/or suffi-cient conditions on the network topology such that consensus can be achieved under properly designed algorithms.It is often reasonable to consider the case when the network topology is deterministic under ideal communication chan-nels.Accordingly,main research on the consensus problem was conducted under a deterministicfixed/switching network topology.That is,the adjacency matrix A(t)is deterministic. Some other times,when considering random communication failures,random packet drops,and communication channel instabilities inherited in physical communication channels,it is necessary and important to study consensus problem in the stochastic setting where a network topology evolves according to some random distributions.That is,the adjacency matrix A(t)is stochastically evolving.In the deterministic setting,consensus is said to be achieved if all agents eventually reach agreement on a common state. In the stochastic setting,consensus is said to be achieved almost surely(respectively,in mean-square or in probability)if all agents reach agreement on a common state almost surely (respectively,in mean-square or with probability one).Note that the problem studied in the stochastic setting is slightly different from that studied in the deterministic setting due to the different assumptions in terms of the network topology. Consensus over a stochastic network topology was perhaps first studied in[27],where some sufficient conditions on the network topology were given to guarantee consensus with probability one for systems with single-integrator kinemat-ics(1),where the rate of convergence was also studied.Further results for consensus under a stochastic network topology were reported in[28]–[30],where research effort was conducted for systems with single-integrator kinematics[28],[29]or double-integrator dynamics[30].Consensus for single-integrator kine-matics under stochastic network topology has been exten-sively studied in particular,where some general conditions for almost-surely consensus was derived[29].Loosely speaking, almost-surely consensus for single-integrator kinematics can be achieved,i.e.,x i(t)−x j(t)→0almost surely,if and only if the expectation of the network topology,namely,the network topology associated with expectation E[A(t)],has a directed spanning tree.It is worth noting that the conditions are analogous to that in[9],[10],but in the stochastic setting. In view of the special structure of the closed-loop systems concerning consensus for single-integrator kinematics,basic properties of the stochastic matrices play a crucial role in the convergence analysis of the associated control algorithms. Consensus for double-integrator dynamics was studied in[30], where the switching network topology is assumed to be driven by a Bernoulli process,and it was shown that consensus can be achieved if the union of all the graphs has a directed spanning tree.Apparently,the requirement on the network topology for double-integrator dynamics is a special case of that for single-integrator kinematics due to the difference nature of thefinal states(constantfinal states for single-integrator kinematics and possible dynamicfinal states for double-integrator dynamics) caused by the substantial dynamical difference.It is still an open question as if some general conditions(corresponding to some specific algorithms)can be found for consensus with double-integrator dynamics.In addition to analyzing the conditions on the network topology such that consensus can be achieved,a special type of consensus algorithm,the so-called gossip algorithm[31],[32], has been used to achieve consensus in the stochastic setting. The gossip algorithm can always guarantee consensus almost surely if the available pairwise communication channels satisfy certain conditions(such as a connected graph).The way of network topology switching does not play any role in the consideration of consensus.The current study on consensus over stochastic network topologies has shown some interesting results regarding:(1) consensus algorithm design for various multi-agent systems,(2)conditions of the network topologies on consensus,and(3)effects of the stochastic network topologies on the con-vergence rate.Future research on this topic includes,but not limited to,the following two directions:(1)when the network topology itself is stochastic,how to determine the probability of reaching consensus almost surely?(2)compared with the deterministic network topology,what are the advantages and disadvantages of the stochastic network topology,regarding such as robustness and convergence rate?As is well known,disturbances and uncertainties often exist in networked systems,for example,channel noise,commu-nication noise,uncertainties in network parameters,etc.In addition to the stochastic network topologies discussed above, the effect of stochastic disturbances[33],[34]and uncertain-ties[35]on the consensus problem also needs investigation. Study has been mainly devoted to analyzing the performance of consensus algorithms subject to disturbances and to present-ing conditions on the uncertainties such that consensus can be achieved.In addition,another interesting direction in dealing with disturbances and uncertainties is to design distributed localfiltering algorithms so as to save energy and improve computational efficiency.Distributed localfiltering algorithms play an important role and are more effective than traditional centralizedfiltering algorithms for multi-agent systems.For example,in[36]–[38]some distributed Kalmanfilters are designed to implement data fusion.In[39],by analyzing consensus and pinning control in synchronization of complex networks,distributed consensusfiltering in sensor networks is addressed.Recently,Kalmanfiltering over a packet-dropping network is designed through a probabilistic approach[40]. Today,it remains a challenging problem to incorporate both dynamics of consensus and probabilistic(Kalman)filtering into a unified framework.plex Dynamical SystemsSince consensus is concerned with the behavior of a group of vehicles,it is natural to consider the system dynamics for practical vehicles in the study of the consensus problem. Although the study of consensus under various system dynam-ics is due to the existence of complex dynamics in practical systems,it is also interesting to observe that system dynamics play an important role in determining thefinal consensus state.For instance,the well-studied consensus of multi-agent systems with single-integrator kinematics often converges to a constantfinal value instead.However,consensus for double-integrator dynamics might admit a dynamicfinal value(i.e.,a time function).These important issues motivate the study of consensus under various system dynamics.As a direct extension of the study of the consensus prob-lem for systems with simple dynamics,for example,with single-integrator kinematics or double-integrator dynamics, consensus with general linear dynamics was also studied recently[41]–[43],where research is mainly devoted tofinding feedback control laws such that consensus(in terms of the output states)can be achieved for general linear systems˙x i=Ax i+Bu i,y i=Cx i,(3) where A,B,and C are constant matrices with compatible sizes.Apparently,the well-studied single-integrator kinematics and double-integrator dynamics are special cases of(3)for properly choosing A,B,and C.As a further extension,consensus for complex systems has also been extensively studied.Here,the term consensus for complex systems is used for the study of consensus problem when the system dynamics are nonlinear[44]–[48]or with nonlinear consensus algorithms[49],[50].Examples of the nonlinear system dynamics include:•Nonlinear oscillators[45].The dynamics are often as-sumed to be governed by the Kuramoto equation˙θi=ωi+Kstability.A well-studied consensus algorithm for(1)is given in(2),where it is now assumed that time delay exists.Two types of time delays,communication delay and input delay, have been considered in the munication delay accounts for the time for transmitting information from origin to destination.More precisely,if it takes time T ij for agent i to receive information from agent j,the closed-loop system of(1)using(2)under afixed network topology becomes˙x i(t)=nj=1a ij(t)[x j(t−T ij)−x i(t)].(7)An interpretation of(7)is that at time t,agent i receives information from agent j and uses data x j(t−T ij)instead of x j(t)due to the time delay.Note that agent i can get its own information instantly,therefore,input delay can be considered as the summation of computation time and execution time. More precisely,if the input delay for agent i is given by T p i, then the closed-loop system of(1)using(2)becomes˙x i(t)=nj=1a ij(t)[x j(t−T p i)−x i(t−T p i)].(8)Clearly,(7)refers to the case when only communication delay is considered while(8)refers to the case when only input delay is considered.It should be emphasized that both communication delay and input delay might be time-varying and they might co-exist at the same time.In addition to time delay,it is also important to consider packet drops in exchanging state information.Fortunately, consensus with packet drops can be considered as a special case of consensus with time delay,because re-sending packets after they were dropped can be easily done but just having time delay in the data transmission channels.Thus,the main problem involved in consensus with time delay is to study the effects of time delay on the convergence and performance of consensus,referred to as consensusabil-ity[52].Because time delay might affect the system stability,it is important to study under what conditions consensus can still be guaranteed even if time delay exists.In other words,can onefind conditions on the time delay such that consensus can be achieved?For this purpose,the effect of time delay on the consensusability of(1)using(2)was investigated.When there exists only(constant)input delay,a sufficient condition on the time delay to guarantee consensus under afixed undirected interaction graph is presented in[8].Specifically,an upper bound for the time delay is derived under which consensus can be achieved.This is a well-expected result because time delay normally degrades the system performance gradually but will not destroy the system stability unless the time delay is above a certain threshold.Further studies can be found in, e.g.,[53],[54],which demonstrate that for(1)using(2),the communication delay does not affect the consensusability but the input delay does.In a similar manner,consensus with time delay was studied for systems with different dynamics, where the dynamics(1)are replaced by other more complex ones,such as double-integrator dynamics[55],[56],complex networks[57],[58],rigid bodies[59],[60],and general nonlinear dynamics[61].In summary,the existing study of consensus with time delay mainly focuses on analyzing the stability of consensus algo-rithms with time delay for various types of system dynamics, including linear and nonlinear dynamics.Generally speaking, consensus with time delay for systems with nonlinear dynam-ics is more challenging.For most consensus algorithms with time delays,the main research question is to determine an upper bound of the time delay under which time delay does not affect the consensusability.For communication delay,it is possible to achieve consensus under a relatively large time delay threshold.A notable phenomenon in this case is that thefinal consensus state is constant.Considering both linear and nonlinear system dynamics in consensus,the main tools for stability analysis of the closed-loop systems include matrix theory[53],Lyapunov functions[57],frequency-domain ap-proach[54],passivity[58],and the contraction principle[62]. Although consensus with time delay has been studied extensively,it is often assumed that time delay is either constant or random.However,time delay itself might obey its own dynamics,which possibly depend on the communication distance,total computation load and computation capability, etc.Therefore,it is more suitable to represent the time delay as another system variable to be considered in the study of the consensus problem.In addition,it is also important to consider time delay and other physical constraints simultaneously in the study of the consensus problem.D.QuantizationQuantized consensus has been studied recently with motiva-tion from digital signal processing.Here,quantized consensus refers to consensus when the measurements are digital rather than analog therefore the information received by each agent is not continuous and might have been truncated due to digital finite precision constraints.Roughly speaking,for an analog signal s,a typical quantizer with an accuracy parameterδ, also referred to as quantization step size,is described by Q(s)=q(s,δ),where Q(s)is the quantized signal and q(·,·) is the associated quantization function.For instance[63],a quantizer rounding a signal s to its nearest integer can be expressed as Q(s)=n,if s∈[(n−1/2)δ,(n+1/2)δ],n∈Z, where Z denotes the integer set.Note that the types of quantizers might be different for different systems,hence Q(s) may differ for different systems.Due to the truncation of the signals received,consensus is now considered achieved if the maximal state difference is not larger than the accuracy level associated with the whole system.A notable feature for consensus with quantization is that the time to reach consensus is usuallyfinite.That is,it often takes afinite period of time for all agents’states to converge to an accuracy interval.Accordingly,the main research is to investigate the convergence time associated with the proposed consensus algorithm.Quantized consensus was probablyfirst studied in[63], where a quantized gossip algorithm was proposed and its convergence was analyzed.In particular,the bound of theconvergence time for a complete graph was shown to be poly-nomial in the network size.In[64],coding/decoding strate-gies were introduced to the quantized consensus algorithms, where it was shown that the convergence rate depends on the accuracy of the quantization but not the coding/decoding schemes.In[65],quantized consensus was studied via the gossip algorithm,with both lower and upper bounds of the expected convergence time in the worst case derived in terms of the principle submatrices of the Laplacian matrix.Further results regarding quantized consensus were reported in[66]–[68],where the main research was also on the convergence time for various proposed quantized consensus algorithms as well as the quantization effects on the convergence time.It is intuitively reasonable that the convergence time depends on both the quantization level and the network topology.It is then natural to ask if and how the quantization methods affect the convergence time.This is an important measure of the robustness of a quantized consensus algorithm(with respect to the quantization method).Note that it is interesting but also more challenging to study consensus for general linear/nonlinear systems with quantiza-tion.Because the difference between the truncated signal and the original signal is bounded,consensus with quantization can be considered as a special case of one without quantization when there exist bounded disturbances.Therefore,if consensus can be achieved for a group of vehicles in the absence of quantization,it might be intuitively correct to say that the differences among the states of all vehicles will be bounded if the quantization precision is small enough.However,it is still an open question to rigorously describe the quantization effects on consensus with general linear/nonlinear systems.E.RemarksIn summary,the existing research on the consensus problem has covered a number of physical properties for practical systems and control performance analysis.However,the study of the consensus problem covering multiple physical properties and/or control performance analysis has been largely ignored. In other words,two or more problems discussed in the above subsections might need to be taken into consideration simul-taneously when studying the consensus problem.In addition, consensus algorithms normally guarantee the agreement of a team of agents on some common states without taking group formation into consideration.To reflect many practical applications where a group of agents are normally required to form some preferred geometric structure,it is desirable to consider a task-oriented formation control problem for a group of mobile agents,which motivates the study of formation control presented in the next section.IV.F ORMATION C ONTROLCompared with the consensus problem where thefinal states of all agents typically reach a singleton,thefinal states of all agents can be more diversified under the formation control scenario.Indeed,formation control is more desirable in many practical applications such as formationflying,co-operative transportation,sensor networks,as well as combat intelligence,surveillance,and reconnaissance.In addition,theperformance of a team of agents working cooperatively oftenexceeds the simple integration of the performances of all individual agents.For its broad applications and advantages,formation control has been a very active research subject inthe control systems community,where a certain geometric pattern is aimed to form with or without a group reference.More precisely,the main objective of formation control is to coordinate a group of agents such that they can achievesome desired formation so that some tasks can befinished bythe collaboration of the agents.Generally speaking,formation control can be categorized according to the group reference.Formation control without a group reference,called formationproducing,refers to the algorithm design for a group of agents to reach some pre-desired geometric pattern in the absenceof a group reference,which can also be considered as the control objective.Formation control with a group reference,called formation tracking,refers to the same task but followingthe predesignated group reference.Due to the existence of the group reference,formation tracking is usually much morechallenging than formation producing and control algorithmsfor the latter might not be useful for the former.As of today, there are still many open questions in solving the formationtracking problem.The following part of the section reviews and discussesrecent research results and progress in formation control, including formation producing and formation tracking,mainlyaccomplished after2006.Several milestone results prior to 2006can be found in[69]–[71].A.Formation ProducingThe existing work in formation control aims at analyzingthe formation behavior under certain control laws,along with stability analysis.1)Matrix Theory Approach:Due to the nature of multi-agent systems,matrix theory has been frequently used in thestability analysis of their distributed coordination.Note that consensus input to each agent(see e.g.,(2))isessentially a weighted average of the differences between the states of the agent’s neighbors and its own.As an extensionof the consensus algorithms,some coupling matrices wereintroduced here to offset the corresponding control inputs by some angles[72],[73].For example,given(1),the controlinput(2)is revised as u i(t)= n j=1a ij(t)C[x j(t)−x i(t)], where C is a coupling matrix with compatible size.If x i∈R3, then C can be viewed as the3-D rotational matrix.The mainidea behind the revised algorithm is that the original controlinput for reaching consensus is now rotated by some angles. The closed-loop system can be expressed in a vector form, whose stability can be determined by studying the distribution of the eigenvalues of a certain transfer matrix.Main research work was conducted in[72],[73]to analyze the collective motions for systems with single-integrator kinematics and double-integrator dynamics,where the network topology,the damping gain,and C were shown to affect the collective motions.Analogously,the collective motions for a team of nonlinear self-propelling agents were shown to be affected by。

18659177_非洲Muglad多旋回陆内被动裂谷盆地演化及其控油气作用

18659177_非洲Muglad多旋回陆内被动裂谷盆地演化及其控油气作用

1000 0569/2019/035(04) 1194 12ActaPetrologicaSinica 岩石学报doi:10 18654/1000 0569/2019 04 14非洲Muglad多旋回陆内被动裂谷盆地演化及其控油气作用张光亚1 黄彤飞1 刘计国1 余朝华1 赵岩2 刘爱香1 客伟利1 王彦奇1ZHANGGuangYa1,HUANGTongFei1,LIUJiGuo1,YUZhaoHua1,ZHAOYan1,LIUAiXiang1,KEWeiLi1andWANGYanQi11 中国石油天然气股份有限公司勘探开发研究院,北京 1000832 中国科学院地质与地球物理研究所,北京 1000291 PetroChinaResearchInstituteofPetroleumExplorationandDevelopment(RIPED),Beijing100083,China2 InstituteofGeologyandGeophysics,ChineseAcademyofSciences,Beijing100029,China2018 12 25收稿,2019 02 19改回ZhangGY,HuangTF,LiuJG,YuZH,ZhaoY,LiuAX,KeWLandWangYQ 2019 Multi cycleevolutionoftheintracontinentalpassiveriftbasinsanditscontrollingonaccumulationofoil&gas:TakingMugladBasininAfricaasanexample ActaPetrologicaSinica,35(4):1194-1212,doi:10 18654/1000 0569/2019 04 14Abstract MugladBasin,oneoftheinteriorpassiveriftbasinsinAfrica,hasexperiencedmulti cyclepassiveriftingandsuperimpositionevolution,whichdistinguishesitselffromtheactiveriftorsingle cyclepassiveriftortypicalmulti cyclesuperimposedbasins Byapplicationofanalysisworkflows&approachestothesuperimposedbasins,includingtheidentificationofkeygeologicaleventsduringtheevolutionaryprocessesandstagedivisionoftheevolutionaryhistory,theproto typebasinsatthekeyperiodswererestored Andbasedontheanalysisonthespatiotemporaldifferenceinriftingintensities,superimpositionprocesses&styles,thesuperimpositiontypesofeachdepressionorsagaswellasitsaccumulationmodesofoil&gaswereestablished ResultsshowthataccompanyingwiththebreakupofGondwana,andevolutionofAtlanticOcean,IndianOceanandRedSeasurroundingtheAfricaPlate,MugladBasinhasexperiencedthreeevolutionaryperiods,namely,thedepositionperiodofAbuGabraFormation(AGFormationforshort)intheEarlyCretaceous,thedepositionperiodofDarfurGroupintheLateCretaceous,andthedepositionperiodofTendiFormationintheCenozoic Theproto typebasinatEarlyCretaceousfeaturesseveralseparategrabensandhalf grabens,whichwasproducedundertheextensionalenvironmenthavingacloserelationshipwiththespreadingofAtlanticOcean;thepro typebasinatLateCretaceousfeaturesthesuccessivedevelopmentofthoseearlygrabensandhalf grabens,whichwasproducedundertheextensionalenvironmenthavingacloserelationshipwiththerapidmovementofIndianPlate Andtheproto typebasinsattheCenozoicweremainlyconfinedwithinthegrabensandhalf grabensinKaikangDepression,whichwaslargelyaffectedbytheopeningofRedSea Accordingtothedifferentintensitiesofthree cycleriftingineachdepressionorsagandthedistinctiveprocessesoftectonicsubsidenceandsedimentfilling,thesuperimpositiontypesofthree cycleriftingweredividedintothreetypes,namely,theearly developed,thesuccessiveandthedynamic Andtheearly developedsagcouldberepresentedbytheSufyanSag,whichfeaturesthedrasticallydecreasingintensityofthree cyclerifting Inthosesags,theamountofbasementsubsidencesandsedimentfillingsduringthefirst cycleriftingandpost riftingcouldaccountfor79%~82%ofthetotalsubsidencesandfillings Andthethirdcycleofriftingandpost riftingwassoweakthatitwasdifficulttointerpretthelayersinseismicsection,andeveninthelogging,itwasalwaysomitted FulaSagwasthemosttypicalsagofthesuccessive Thosesagsfeaturethegraduallydecreasingintensityofthree cyclerifting&post rifting Unliketheformerone,thesecondcycleofrifting&post riftingstillremainsquitestronginintensity,whichcouldbeprovedbythefactthethicknessofDarfurGroup(LateCretaceous)inFulaSagislargerthanthatofBentiuFormation(EarlyCretaceous)whichwasdepositedduringthefirstcycleofpost rifting KaikangDepressionwasthemosttypicaldepressionofthedynamic,whichfeaturestherelativelycontinuousintensityofthethreecycles Whencomparingwiththeformers,everycycleofthethreecyclesintheKaikang本文受中国石油集团重大科技专项(2015D 0909)资助.第一作者简介:张光亚,男,1962年生,博士,教授级高级工程师,博士生导师,主要从事含油气盆地构造与油气地质综合研究,E mail:zgy@petrochina.com.cnDepressionwaslargerthananyoftheearly developedandthesuccessive Eveninthethirdcycleofrifting&post rifting,theamountofsubsidenceandsedimentfillingswasasmuchas2,000m Thespatiotemporaldifferencesinintensitiesofthree cyclerifting&post riftingdeterminethedifferencesinpetroleumgeologicalconditionsforhydrocarbonaccumulationanddistribution Thedominantplayintheearly developedsagsisthelowerplay,andthatinthesuccessivesagsisthemiddleplay However,theupperplayswerethemostdominantplaysinthosedynamicsags Thestudyofmulti cyclesuperimposedpassiveriftbasininthispaperwouldnotonlycontributeandenrichtheresearchonthestructuralfeature,evolutionaryhistoryaswellasitseffectonthehydrocarbonaccumulationofotherriftbasinsintheworld,butalsohadapracticalsignificanceinmakingfurtherstrategiesforexplorationinthesebasinsKeywords Africa;MugladBasin;Break upoftheGondwanaContinent;Passiverifting;Multi cycle;Superimposedbasin;Distributionofoil&gas;Cretaceous Cenozoic摘 要 非洲Muglad盆地经历多旋回陆内被动裂谷发育与叠合演化历史,具有不同于主动裂谷盆地、单旋回被动裂谷盆地以及跨越多个变革期的叠合盆地的演化特征。

控罗吉1756隔离分析输入输出模块系列说明书

控罗吉1756隔离分析输入输出模块系列说明书

ControlLogix 1756 Isolated Analog I/O ModulesEnhanced I/O for Advanced Control ApplicationsEnhanced Analog I/O ModulesThree 8-channel isolated designs and 12-channel and 16-channelnon-isolated designs with improved functionality of analog I/O provide faster performance, more accuracy, better resolution and cost savings due to less space needed in the chassis for additional modules and power supplies.• 1756-IF8I General Purpose Isolated Analog Input ModuleThis general purpose isolated analog input module provides faster performance, accuracy and per channel configuration for voltage, current or 2-wire transmitter current sourcing.• 1756-IRT8I Combined Temperature Sensing Input ModuleThis combined temperature sensing input (Thermocouple and RTD) module provides faster performance, accuracy and per channel configuration for either RTD or Thermocouple.• 1756-OF8I General Purpose Current Voltage Analog Output Module This general purpose current/voltage analog output module provides faster performance, accuracy and per channel configuration for either current or voltage.• 1756-IR12 non-Isolated High Density RTD module • 1756-IT16 non-Isolated High Density Temperature module •1756-CJC Cold Junction Compensation kit for use with either 1756-IRT8I or 1756-IT16 module. Kit includes two jumpersFeatures and Benefits of the ControlLogix® 1756 Isolated Analog I/O Modules:• Provides increased accuracy,repeatability and stability over the entire temperature operating range for enhanced precision • Up to 24 bits of usable resolution for increased precision • 1 ms of input sampling of floating point values for faster output response times helping to enable higher performance • Offers industry standard 8-point channel density enabling the ability to wire more devices per module for hardware simplification • No field calibration required for simplified device replacement and faster installation • Synchronized input sampling for increased visibility across the system for real-time control over the EtherNet/IP network• Per channel status and fault statusindicator annunciation for more simplified troubleshooting and maintenance • SIL 1 Systematic Capability 2 Type certified for use in a ControlLogix SIL 2 architecture • Emulation mode helps enable customers to more seamlesslymigrate from 6-channel applicationsAllen-Bradley, ControlLogix, LISTEN. THINK. SOLVE. and Rockwell Software are trademarks of Rockwell Automation, Inc. Trademarks not belonging to Rockwell Automation are property of their respective companies.The specifications for the 1756-IF8I, 1756-IRT8I, 1756-OF8I, 1756-IR12 and 1756-IT16 include:Publication1756-PP020C-EN-E – May 2016Copyright © 2016 Rockwell Automation, Inc. All Rights Reserved. Printed in USA.Supersedes Publication 1756-PP020B-EN-E – May 2015Analog 8-Channel Wiring SystemThe wiring system solution for the 1756 8-channel analog I/O modules enables the wiring of more devices. The 6-channel wiring system also functions with the 8-point I/O modules, allowing the preservation of existing field terminations.• Significantly decreases wiring time from the controller card to the terminal blocks• Provides additional capabilities for connections to the controller card via fusing and relays • Provides a more standard connection terminal block。

SMC 流量控制器用户手册说明书

SMC 流量控制器用户手册说明书

Instruction Manual Flow Controller for AirIN502-44-# / IN502-45-# seriesThe intended use of the flow controller is to monitor and display flow information with the optional connection to IO-Link communication.These safety instructions are intended to prevent hazardous situations and/or equipment damage. These instructions indicate the level of potential hazard with the labels of “Caution,” “Warning” or “Danger.” They are all important notes for safety and must be followed in addition to International Standards (ISO/IEC) *1), and other safety regulations. *1)ISO 4414: Pneumatic fluid power - General rules relating to systems. ISO 4413: Hydraulic fluid power - General rules relating to systems.IEC 60204-1: Safety of machinery - Electrical equipment of machines. (Part 1: General requirements)ISO 10218-1: Manipulating industrial robots -Safety. etc.• Refer to product catalogue, Operation Manual and Handling Precautions for SMC Products for additional information. • Keep this manual in a safe place for future reference.Warning• Always ensure compliance with relevant safety laws and standards.• All work must be carried out in a safe manner by a qualified person in compliance with applicable national regulations.• This product is class A equipment intended for use in an industrial environment. There may be potential difficulties in ensuring electromagnetic compatibility in other environments due to conducted or radiated disturbances.• Refer to the operation manual on the SMC website (URL: https:// ) for more Safety instructions.• Special products (-X) might have specifications different from those shown in the specifications section. Contact SMC for specific drawings.Caution1. When selecting equipment, carefully consider the application, requiredspecifications, and operating conditions (fluid, pressure, flow rate, filtration, and environment), making sure not to exceed the specification range.2. This product is provided for normally typical forms of use in the manufacturing industry. As such, to use the product for applications that may affect the human body directly or indirectly such as caisson shield is not foreseen.3. When the product is used as an air blower for food, install an appropriate filter to eliminate foreign matter in compressed air for air blowing. (Refer to the following example of pneumatic circuit).4. Quality management relating to hygiene for food and medical treatment is not implemented for the product.The product is produced in same line that manufactures other product which uses other materials. In rare cases, some of these materials can be found as a residue. 5. Food grease used• Fluid contact parts: NSF H1 grade grease• Part other than fluid contact parts: NSF H1 grade grease or grease which is not NSF H1 grade6. The grease used in the solenoid valves built into the product is not food grease.Grease may drain out of the product from the solenoid valve EXH. If necessary, pipe it to the outside of the area.7. The product generates particles from the wear of sliding parts inside. When the product is used as an air blower, install an appropriate filter on the outlet of the product to prevent foreign matter from flowing to the downstream. Filters require regular inspection, replacement of the element, and maintenance referring to the operation manual.8. Flush the piping line before using the product for the first time and after it has been replaced. Also, if piping, etc., is to be connected, flush (air blow) before using the product for the first time in order to reduce the effects of the dust generated from the connection, etc. Flushing the line is also required to eliminate contamination resulting from the installation of piping lines. Therefore, be sure to flush the line before running the system.2 Specification2.1 IO-Link specifications (for models with IO-Link)3 Name and function of parts3.1ORIGINAL INSTRUCTIONS3 Name and function of parts (continued)3.2 DisplayPart DescriptionOperation LED LED is ON (orange) when OUT is ON.Main display(red/green)Displays the current controlled flow, setting modestatus, selected display units and error codes.UP buttonSelects the mode and increases the ON/OFF setvalue.SET buttonPress this button to change the mode and toconfirm settings.DOWN buttonChanges the sub display, selects the mode anddecreases the ON/OFF set value.Units display 1(red/green)LED turns ON when STD is selected for thereference condition.Units display 2(red/green)LED indicates the selected flow rate units.Sub display (left) Displays (orange) the display item label.Sub displayDisplays (orange) the display item, setting value,peak/bottom value, etc.IO-Link statusindicator lightDisplays OUT1 output communication status(SIO mode, start-up mode, Pre-operation mode,operation mode) and presence of communicationdata (for products with IO-Link only).•Refer to the operation manual on the SMC website(URL: https://) for more details of the IO-Linkstatus indicator light operation and display.4 Installation4.1 InstallationWarning•Do not install the product unless the safety instructions have been readand understood.•Use the product within the specified operating pressure andtemperature range.4.2 EnvironmentWarning•Do not use in an environment where corrosive gases, chemicals, saltwater, water or steam are present.•Do not use the product in an environment where the product is constantlyexposed to water or oil splashes.•Do not use in an explosive atmosphere.•Do not expose to direct sunlight. Use a suitable protective cover.•Do not install in a location subject to vibration or impact in excess ofthe product’s specifications.•Do not mount in a location exposed to radiant heat that would result intemperatures in excess of the product’s specifications.•Do not use in an area where electrical surges are generated.•Prevent foreign matter such as remnant of wires from entering theproduct4.3 Mounting•Never mount the product in a location where it will be used as afoothold.•Do not mount the product upside down.•Mount the product so that the fluid flows in the direction indicated bythe arrow on the side of the body.•If the EXH port of the solenoid valve may be exposed to water or dust,connect a fitting and tube (sold separately) and route the tube to a safeplace where it will not be affected by water or dust.4 Installation (continued)•Install the product using 4 screws suitable for the product, tightenedaccording to the required tightening torque.•Suitable screw: M5, Tightening torque: 3 N•m ±10%•Screws should be prepared by the user.Refer to the operation manual on the SMC website (URL:https://) for mounting hole details and outlinedimensions.4.4 PipingCaution•Before connecting piping make sure to clean up chips, cutting oil, dustetc.•When installing piping or fittings, ensure sealant material does notenter inside the port.•Tighten the piping to the correct tightening torque: 20 to 25 N•mIf the tightening torque is exceeded, the product can be damaged.If the tightening torque is insufficient, the connection threads andbrackets may become loose.•Confirm that there is no leakage after piping.•When attaching a fitting, the attachment should be held with a wrench.Holding other parts with a wrench may damage the product.5 Wiring5.1 WiringCaution•Connections should only be made with the power supply turned off.•Use a separate route for the product wiring. If wires and cables arerouted together with power or high voltage cables, malfunction mayresult due to noise.•If a commercially available switching power supply is used, be sure toground the frame ground (FG) terminal. If a switch-mode power supplyis connected for use, switching noise will be superimposed and theproduct will not be able to meet the specifications. In that case, inserta noise filter such as a line noise filter/ferrite between the switchingpower supply and the product, or change the switching power supplyto a series power supply.5 Wiring (continued)5.2 Connector installation / removal•Align the lead wire M12 connector with the connector key groove onthe controller, and insert it straight in. Turn the knurled part clockwise.Connection is complete when the knurled part is fully tightened. Checkthat the connection is not loose.•To unplug the connector, loosen the knurled part and pull it straight out.Connector pin layoutWhen used as a Switch output deviceNo. NameWirecolourFunction1 DC(+) Brown 24 VDC2 An IN White Analogue input3 DC(-) Blue 0 V4 OUT Black Switch output5 An OUT Grey Analogue outputWhen used as an IO-Link deviceNo. NameWirecolourFunction1 L(+) Brown 24 VDC2 An IN White Analogue input3 L(-) Blue 0 V4 C/Q BlackIO-Linkcommunication5N.C. /An OUTGreyN.C. or Analogueoutput.6 Outline of SettingsPower is suppliedRefer to the operation manual on the SMC website (URL:https://) for further Setting details.7 Initial Settings•Configure the reference condition, unit of pressure display, and switchoutput PNP/NPN switch.•Reference conditionStandard condition or normal condition can be selected for thestandard reference condition of flow rate.Standard condition: flow rate converted into volume at 20 °C and 101.3kPa (absolute pressure).Normal condition: flow rate converted into volume at 0 °C and 101.3kPa (absolute pressure).•Units selection functionThe flow rate display units selection function allows for selecting L/minor cfm (ft3/min) as the standard unit.The pressure units selection function allows for selecting kPa, MPa,kgf/cm2, bar, or psi as the standard unit.This setting is only available for models with the units selection function.•Switch output typeThe switch output function can be toggled between PNP and NPNoutput.8 Function Selection modeIn measurement mode, press the SET button for at least 1 second but nomore than 3 seconds to display [F 0].The mode in which [F□□] is displayed and changes to the respectivefunction settings are made is referred to as function selection mode.Press the SET button for 2 seconds or longer in function selection modeto return to measurement mode.Note: Some functions are not supported on models with specific productnumbers. [---] will be displayed on the sub display (right) for functions thatare not supported or cannot be selected due to other settings.8.1 Default settings•The factory default settings are as follows.If these settings are acceptable, retain for use.To change a setting, enter function selection mode.•[F 0] Reference condition, unit of pressure display, and switch outputPNP/NPN.Item Default settingReference condition Standard conditionFlow rate display unit L/minPressure display unit kPaSwitch output PNP/NPN switch PNP•[F 1] Setting of OUT1Item Description Default settingOutputmodeLimit deviation tolerance mode, erroroutput mode, or switch output off canbe selected.Limit deviationtolerancemodeReverseoutputSelects which switch output is used,Normal or Reverse.Normal outputLimitdeviationtoleranceSets the switch output on or off whenmeasured flow rate is within the limitdeviation tolerance of set flow rate.±2% F.S.ON delaytimeDelay time (rising) of switch outputcan be selected.0.00 sec.OFF delaytimeDelay time of (falling) switch outputcan be selected.0.00 sec.DisplaycolourSelect the display colour.Output ON:GreenOutput OFF:RedThe product code is displayed for approximately 3 seconds afterpower is supplied. Then, measurement mode is displayed.*: Switch operation starts within approx. 0.2 seconds after power is supplied.[Initial Settings]Set the reference condition, unit of pressure display, and switchoutput PNP/NPN switch.[Function Selection mode]Each function setting can bechanged.[Measurement mode]In this mode, flow rate control and display and switch operationsare performed in accordance with commanded flow rates.This is the basic mode; other modes should be selected for set-point changes and other function settings.[Other Settings]•Zero clear•Key lock• Other Function Settings9 Other Settings• Peak / Bottom value display • Zero clear• Key-lock functionRefer to the operation manual on the SMC website (URL: https:// ) for setting these functions. 10 IO-Link parameter setting• IODD fileIODD (I/O Device Description) is a definition file which provides all properties and parameters required for establishing functions and communication of the device.IODD includes the main IODD file and a set of image files such as vendor logo, device picture and device icon. The IODD file list is shown below.*1: "yyyymmdd" indicates the file preparation date. yyyy is the year, mm is the month and dd is the date.• The latest IODD file can be downloaded from the SMC website (https:// ).11 How to OrderRefer to the SMC website (URL: https:// ) for more How to Order details.12 Outline Dimensions (mm)Refer to the SMC website (URL: https:// ) for details of Outline dimensions.13.1 Error indicationIf the error cannot be reset after the above measures are taken, or errors other than the above are displayed, please contact SMC.14.1 General MaintenanceCaution• Not following proper maintenance procedures could cause the product to malfunction and lead to equipment damage.• If handled improperly, compressed air can be dangerous.• Maintenance of pneumatic systems should be performed only by qualified personnel.• Before performing maintenance, turn off the power supply and be sure to cut off the supply pressure. Confirm that the air is released to atmosphere.• After installation and maintenance, apply operating pressure and power to the equipment and perform appropriate functional and leakage tests to make sure the equipment is installed correctly.• If any electrical connections are disturbed during maintenance, ensure they are reconnected correctly and safety checks are carried out as required to ensure continued compliance with applicable national regulations.• Do not make any modification to the product.• Do not disassemble the product, unless required by installation or maintenance instructions.• How to reset the product after a power cut or when the power has been unexpectedly removedThe settings for the product are retained in memory prior to the power loss or de-energizing of the product.The output condition is also recoverable to that prior to the power loss or de-energizing. However, this may change depending on the operating environment. Therefore, check the safety of the whole installation before operating the product.If the installation is using accurate control, wait until the product has warmed up (approximately 10 to 15 minutes) before operation.15 Limitations of Use15.1 Limited warranty and Disclaimer/Compliance Requirements Refer to Handling Precautions for SMC Products.16 Product disposalThis product should not be disposed of as municipal waste. Check your local regulations and guidelines to dispose of this product correctly, in order to reduce the impact on human health and the environment.17 ContactsRefer to or www.smc.eu for your local distributor / importer.URL: https:// (Global) https://www.smc.eu (Europe) SMC Corporation, 4-14-1, Sotokanda, Chiyoda-ku, Tokyo 101-0021, Japan Specifications are subject to change without prior notice from the manufacturer. © 2022-2023 SMC Corporation All Rights Reserved. Template DKP50047-F-085M。

数学英文论文

数学英文论文

070451 Controlling chaos based on an adaptive nonlinear compensatingmechanism*Corresponding author,Xu Shu ,email:123456789@Abstract The control problems of chaotic systems are investigated in the presence of parametric u ncertainty and persistent external distu rbances based on nonlinear control theory. B y designing a nonlinear compensating mechanism, the system deterministic nonlinearity, parametric uncertainty and disturbance effect can be compensated effectively. The renowned chaotic Lorenz system subject to parametric variations and external disturbances is studied as an illustrative example. From Lyapu nov stability theory, sufficient conditions for the choice of control parameters are derived to guarantee chaos control. Several groups of experiments are carried out, including parameter change experiments, set-point change experiments and disturbance experiments. Simulation results indicate that the chaotic motion can be regulated not only to stead y states but also to any desired periodic orbits with great immunity to parametric variations and external distu rbances.Keywords: chaotic system, nonlinear compensating mechanism, Lorenz chaotic systemPACC: 05451. IntroductionChaotic motion, as the peculiar behavior in deterministic systems, may be undesirable in many cases, so suppressing such a phenomenon has been intensively studied in recent years. Generally speaking chaos suppression and chaos synchronization[1-4 ]are two active research fields in chaos control and are both crucial in application of chaos. In the following letters we only deal with the problem of chaos suppression and will not discuss the chaos synchronization problem.Since the early 1990s, the small time-dependent parameter perturbation was introduced by Ott,Grebogi, and Y orke to eliminate chaos,[5]many effective control methods have been reported in various scientific literatures.[1-4,6-36,38-44,46] There are two lines in these methods. One is to introduce parameter perturbations to an accessible system parameter, [5-6,8-13] the other is to introduce an additive external force to the original uncontrolled chaotic system. [14-37,39-43,47] Along the first line, when system parameters are not accessible or can not be changed easily, or the environment perturbations are not avoided, these methods fail. Recently, using additive external force to achieve chaos suppression purpose is in the ascendant. Referring to the second line of the approaches, various techniques and methods have been proposed to achieve chaos elimination, to mention only a few:(ⅰ) linear state feedback controlIn Ref.[14] a conventional feedback controller was designed to drive the chaotic Duffing equation to one of its inherent multiperiodic orbits.Recently a linear feedback control law based upon the Lyapunov–Krasovskii (LK) method was developed for the suppression of chaotic oscillations.[15]A linear state feedback controller was designed to solve the chaos control problem of a class of new chaotic system in Ref.[16].(ⅱ) structure variation control [12-16]Since Y u X proposed structure variation method for controlling chaos of Lorenz system,[17]some improved sliding-mode control strategies were*Project supported by the National Natural Science Foundation of C hina (Grant No 50376029). †Corresponding au thor. E-mail:zibotll@introduced in chaos control. In Ref.[18] the author used a newly developed sliding mode controller with a time-varying manifold dynamic to compensate the external excitation in chaotic systems. In Ref.[19] the design schemes of integration fuzzy sliding-mode control were addressed, in which the reaching law was proposed by a set of linguistic rules. A radial basis function sliding mode controller was introduced in Ref.[20] for chaos control.(ⅲ) nonlinear geometric controlNonlinear geometric control theory was introduced for chaos control in Ref.[22], in which a Lorenz system model slightly different from the original Lorenz system was studied considering only the Prandtl number variation and process noise. In Ref.[23] the state space exact linearization method was also used to stabilize the equilibrium of the Lorenz system with a controllable Rayleigh number. (ⅳ)intelligence control[24-27 ]An intelligent control method based on RBF neural network was proposed for chaos control in Ref.[24]. Liu H, Liu D and Ren H P suggested in Ref.[25] to use Least-Square Support V ector Machines to drive the chaotic system to desirable points. A switching static output-feedback fuzzy-model-based controller was studied in Ref.[27], which was capable of handling chaos.Other methods are also attentively studied such as entrainment and migration control, impulsive control method, optimal control method, stochastic control method, robust control method, adaptive control method, backstepping design method and so on. A detailed survey of recent publications on control of chaos can be referenced in Refs.[28-34] and the references therein.Among most of the existing control strategies, it is considered essentially to know the model parameters for the derivation of a controller and the control goal is often to stabilize the embedded unstable period orbits of chaotic systems or to control the system to its equilibrium points. In case of controlling the system to its equilibrium point, one general approach is to linearize the system in the given equilibrium point, then design a controller with local stability, which limits the use of the control scheme. Based on Machine Learning methods, such as neural network method[24]or support vector machine method,[25]the control performance often depends largely on the training samples, and sometimes better generalization capability can not be guaranteed.Chaos, as the special phenomenon of deterministic nonlinear system, nonlinearity is the essence. So if a nonlinear real-time compensator can eliminate the effect of the system nonlinearities, chaotic motion is expected to be suppressed. Consequently the chaotic system can be controlled to a desired state. Under the guidance of nonlinear control theory, the objective of this paper is to design a control system to drive the chaotic systems not only to steady states but also to periodic trajectories. In the next section the controller architecture is introduced. In section 3, a Lorenz system considering parametric uncertainties and external disturbances is studied as an illustrative example. Two control schemes are designed for the studied chaotic system. By constructing appropriate L yapunov functions, after rigorous analysis from L yapunov stability theory sufficient conditions for the choice of control parameters are deduced for each scheme. Then in section 4 we present the numerical simulation results to illustrate the effectiveness of the design techniques. Finally some conclusions are provided to close the text.2. Controller architectureSystem differential equation is only an approximate description of the actual plant due to various uncertainties and disturbances. Without loss of generality let us consider a nonlinear continuous dynamic system, which appears strange attractors under certain parameter conditions. With the relative degree r n(n is the dimension of the system), it can be directly described or transformed to the following normal form:121(,,)((,,)1)(,,,)(,,)r r r z z z z za z v wb z v u u d z v u u vc z v θθθθθθθθ-=⎧⎪⎪⎪=⎪=+∆+⎨⎪ ++∆-+⎪⎪ =+∆+⎪=+∆⎩ (1) 1y z =where θ is the parameter vector, θ∆ denotes parameter uncertainty, and w stands for the external disturbance, such that w M ≤with Mbeingpositive.In Eq.(1)1(,,)T r z z z = can be called external state variable vector,1(,,)T r n v v v += called internal state variable vector. As we can see from Eq.(1)(,,,,)(,,)((,,)1)d z v w u a z v w b z v uθθθθθθ+∆=+∆+ ++∆- (2)includes system nonlinearities, uncertainties, external disturbances and so on.According to the chaotic system (1), the following assumptions are introduced in order to establish the results concerned to the controller design (see more details in Ref.[38]).Assumption 1 The relative degree r of the chaotic system is finite and known.Assumption 2 The output variable y and its time derivatives i y up to order 1r -are measurable. Assumption 3 The zero dynamics of the systemis asymptotically stable, i.e.,(0,,)v c v θθ=+∆ is asymptotically stable.Assumption 4 The sign of function(,,)b z v θθ+∆is known such that it is always positive or negative.Since maybe not all the state vector is measurable, also (,,)a z v θθ+∆and (,,)b z v θθ+∆are not known, a controller with integral action is introduced to compensate theinfluenceof (,,,,)d z v w u θθ+∆. Namely,01121ˆr r u h z h z h z d------ (3) where110121112100ˆr i i i r r r r i i ii r i i d k z k k k z kz k uξξξ-+=----++-==⎧=+⎪⎪⎨⎪=----⎪⎩∑∑∑ (4)ˆdis the estimation to (,,,,)d z v w u θθ+∆. The controller parameters include ,0,,1i h i r =- and ,0,,1i k i r =- . Here011[,,,]Tr H h h h -= is Hurwitz vector, such that alleigenvalues of the polynomial121210()rr r P s s h sh s h s h --=+++++ (5)have negative real parts. The suitable positive constants ,0,,1i h i r =- can be chosen according to the expected dynamic characteristic. In most cases they are determined according to different designed requirements.Define 1((,,))r k sign b z v θμ-=, here μstands for a suitable positive constant, and the other parameters ,0,,2i k i r =- can be selected arbitrarily. After011[,,,]Tr H h h h -= is decided, we can tune ,0,,1i k i r =- toachievesatisfyingstaticperformances.Remark 1 In this section, we consider a n-dimensional nonlinear continuous dynamic system with strange attractors. By proper coordinate transformation, it can be represented to a normal form. Then a control system with a nonlinear compensator can be designed easily. In particular, the control parameters can be divided into two parts, which correspond to the dynamic characteristic and the static performance respectively (The theoretic analysis and more details about the controller can be referenced to Ref.[38]).3. Illustrative example-the Lorenz systemThe Lorenz system captures many of the features of chaotic dynamics, and many control methods have been tested on it.[17,20,22-23,27,30,32-35,42] However most of the existing methods is model-based and has not considered the influence ofpersistent external disturbances.The uncontrolled original Lorenz system can be described by112121132231233()()()()x P P x P P x w x R R x x x x w xx x b b x w =-+∆++∆+⎧⎪=+∆--+⎨⎪=-+∆+⎩ (6) where P and R are related to the Prendtl number and Rayleigh number respectively, and b is a geometric factor. P ∆, R ∆and b ∆denote the parametric variations respectively. The state variables, 1x ,2x and 3x represent measures of fluid velocity and the spatial temperature distribution in the fluid layer under gravity , and ,1,2,3i w i =represent external disturbance. In Lorenz system the desired response state variable is 1x . It is desired that 1x is regulated to 1r x , where 1r x is a given constant. In this section we consider two control schemes for system (6).3.1 Control schemes for Lorenz chaotic system3.1.1 Control scheme 1The control is acting at the right-side of the firstequation (1x), thus the controlled Lorenz system without disturbance can be depicted as1122113231231x Px Px u xRx x x x x x x bx y x =-++⎧⎪=--⎨⎪=-⎩= (7) By simple computation we know system (7) has relative degree 1 (i.e., the lowest ordertime-derivative of the output y which is directly related to the control u is 1), and can be rewritten as1122113231231z Pz Pv u vRz z v v v z v bv y z =-++⎧⎪=--⎨⎪=-⎩= (8) According to section 2, the following control strategy is introduced:01ˆu h z d=-- (9) 0120010ˆ-d k z k k z k uξξξ⎧=+⎪⎨=--⎪⎩ (10) Theorem 1 Under Assumptions 1 toAssumptions 4 there exists a constant value *0μ>, such that if *μμ>, then the closed-loop system (8), (9) and (10) is asymptotically stable.Proof Define 12d Pz Pv =-+, Eq.(8) can be easily rewritten as1211323123z d u v Rz z v v vz v bv =+⎧⎪=--⎨⎪=-⎩ (11) Substituting Eq.(9) into Eq.(11) yields101211323123ˆz h z d dv R z z v v v z v bv ⎧=-+-⎪=--⎨⎪=-⎩ (12) Computing the time derivative of d and ˆdand considering Eq.(12) yields12011132ˆ()()dPz Pv P h z d d P Rz z v v =-+ =--+- +-- (13) 0120010000100ˆ-()()ˆ=()d k z k k z k u k d u k d k z k d d k dξξξ=+ =--++ =-- - = (14)Defining ˆdd d =- , we have 011320ˆ()()dd d P h P R z P z v P v P k d=- =+- --+ (15) Then, we can obtain the following closed-loop system101211323123011320()()z h z dvRz z v v v z v bv d Ph PR z Pz v Pv P k d⎧=-+⎪=--⎪⎨=-⎪⎪=+---+⎩ (16) To stabilize the closed-loop system (16), a L yapunovfunction is defined by21()2V ςς=(17)where, ςdenotes state vector ()123,,,Tz v v d, isthe Euclidean norm. i.e.,22221231()()2V z v v dς=+++ (18) We define the following compact domain, which is constituted by all the points internal to the superball with radius .(){}2222123123,,,2U z v v d zv v dM +++≤(19)By taking the time derivative of ()V ςand replacing the system expressions, we have11223322*********01213()()(1)V z z v v v v dd h z v bv k P d R z v P R P h z d P v d P z v d ς=+++ =----++ +++-- (20) For any ()123,,,z v v d U ∈, we have: 222201230120123()()(1)V h z v b v k P dR z v PR Ph z d P v d d ς≤----+ ++++ ++ (21)Namely,12300()(1)22020V z v v dPR Ph R h R P ς⎡⎤≤- ⎣⎦++ - 0 - - 1 - 2⨯00123(1)()2Tb PR Ph P k P z v v d ⎡⎤⎢⎥⎢⎥⎢⎥⎢⎥⎢⎥⎢⎥0 ⎢⎥2⎢⎥++⎢⎥- - - +⎢⎥⎣22⎦⎡⎤⨯ ⎣⎦(22) So if the above symmetrical parameter matrix in Eq.(22) is positive definite, then V is negative and definite, which implies that system (16) is asymptotically stable based on L yapunov stability theory.By defining the principal minor determinants of symmetrical matrix in Eq.(22) as ,1,2,3,4i D i =, from the well-known Sylvester theorem it is straightforward to get the following inequations:100D h => (23)22004RD h =-> (24)23004R b D bh =-> (25)240302001()(1)(2)821[2(1)]08P M D k P D b PR Ph PR D Pb Ph R PR Ph =+-+++--+++>(26)After 0h is determined by solving Inequalities (23) to (25), undoubtedly, the Inequalities (26) can serve effectively as the constraints for the choice of 0k , i.e.20200031(1)(2)821[2(1)]8P M b PR Ph PR D Pb Ph R PR Ph k P D ++++ ++++>- (27)Here,20200*31(1)(2)821[2(1)]8P M b PR Ph PR D Pb Ph R PR Ph P D μ++++ ++++=-.Then the proof of the theorem 1 is completed. 3.1.2 Control scheme 2Adding the control signal on the secondequation (2x ), the system under control can be derived as112211323123x P x P x x R x x x x u xx x bx =-+⎧⎪=--+⎨⎪=-⎩ (28) From Eq.(28), for a target constant 11()r x t x =,then 1()0xt = , by solving the above differential equation, we get 21r r x x =. Moreover whent →∞,3r x converges to 12r x b . Since 1x and 2x havethe same equilibrium, then the measured state can also be chosen as 2x .To determine u , consider the coordinate transform:122133z x v x v x=⎧⎪=⎨⎪=⎩ and reformulate Eq.(28) into the following normal form:1223121231231zRv v v z u vPz Pv v z v bv y z =--+⎧⎪=-⎨⎪=-⎩= (29) thus the controller can be derived, which has the same expression as scheme 1.Theorem 2 Under Assumptions 1, 2, 3 and 4, there exists a constant value *0μ>, such that if *μμ>, then the closed-loop system (9), (10) and (29) is asymptotically stable.Proof In order to get compact analysis, Eq.(29) can be rewritten as12123123z d u v P z P v vz v bv =+⎧⎪=-⎨⎪=-⎩ (30) where 2231d Rv v v z =--Substituting Eq.(9) into Eq.(30),we obtain:1012123123ˆz h z d dv P z P v v z v bv ⎧=-+-⎪=-⎨⎪=-⎩ (31) Giving the following definition:ˆdd d =- (32) then we can get22323112123212301()()()()dRv v v v v z R Pz Pv Pz Pv v v z v bv h z d =--- =--- ----+ (33) 012001000ˆ-()d k z k k z k u k d u k dξξ=+ =--++ = (34) 121232123010ˆ()()()(1)dd d R Pz Pv Pz Pv v v z v bv h z k d=- =--- --+-+ (35)Thus the closed-loop system can be represented as the following compact form:1012123123121232123010()()()(1)zh z d v Pz Pv v z v bv d R Pz Pv Pz Pv v v z v bv h z k d⎧=-+⎪⎪=-⎪=-⎨⎪=---⎪⎪ --+-+⎩(36) The following quadratic L yapunov function is chosen:21()2V ςς=(37)where, ςdenotes state vector ()123,,,Tz v v d , is the Euclidean norm. i.e.,22221231()()2V z v v dς=+++ (38) We can also define the following compact domain, which is constituted by all the points internalto the super ball with radius .(){}2222123123,,,2U z v v d zv v dM =+++≤ (39)Differentiating V with respect to t and using Eq.(36) yields112233222201230011212322321312()(1)(1)()V z z v v v v dd h z P v bv k dP R h z d P z v z v v P b v v d P v d P z v d z v d ς=+++ =----+ +++++ ++--- (40)Similarly, for any ()123,,,z v v d U ∈, we have: 2222012300112133231()(1)(1)(2V h z P v b v k dPR h z d P z v v P b d P v d d M z dς≤----+ +++++ ++++ + (41)i.e.,12300()(12)22V z v v dPR M h P h P Pς⎡⎤≤- ⎣⎦+++ - -2 - 0 ⨯ 001230(12)(1)2TP b PR M h P k z v v d ⎡⎤⎢⎥⎢⎥⎢⎥ - ⎢⎥⎢⎥⎢⎥ ⎢⎥22⎢⎥⎢⎥ +++ - - -+⎢⎥⎣22⎦⎡⎤⨯ ⎣⎦(42) For brevity, Let1001(12)[(222)82(23)]P PR M h b PR P h M P b α=++++++ ++(43) 2201[(231)(13)]8P M P b b PR h α=+-+++ (44)230201(2)[2(12)8(2)(4)]PM P b P P PR M h P b Ph P α=++ +++ ++- (45)Based on Sylvester theorem the following inequations are obtained:100D h => (46)22004PD h P =-> (47)3202PMD bD =-> (48)403123(1)0D k D ααα=+---> (49)where,1,2,3,4i D i =are the principal minordeterminants of the symmetrical matrix in Eq.(42).*0k μ>*12331D αααμ++=- (50)The theorem 2 is then proved.Remark 2 In this section we give two control schemes for controlling chaos in Lorenz system. For each scheme the control depends on the observed variable only, and two control parameters are neededto be tuned, viz. 0h and 0k . According to L yapunov stability theory, after 0h is fixed, the sufficient condition for the choice of parameter 0k is also obtained.4. Simulation resultsChoosing 10P =,28R =, and 8/3b =, the uncontrolled Lorenz system exhibits chaotic behavior, as plotted in Fig.1. In simulation let the initial values of the state of thesystembe 123(0)10,(0)10,(0)10x x x ===.x1x 2x1x 3Fig.1. C haotic trajectories of Lorenz system (a) projected on12x x -plane, (b) projected on 13x x -plane4.1 Simulation results of control the trajectory to steady stateIn this section only the simulation results of control scheme 2 are depicted. The simulation results of control scheme 1 will be given in Appendix. For the first five seconds the control input is not active, at5t s =, control signal is input and the systemtrajectory is steered to set point2121(,,)(8.5,8.5,27.1)T Tr r r x x x b =, as can be seen inFig.2(a). The time history of the L yapunov function is illustrated in Fig.2(b).t/sx 1,x 2,x 3t/sL y a p u n o v f u n c t i o n VFig.2. (a) State responses under control, (b) Time history of the Lyapunov functionA. Simulation results in the presence ofparameters ’ changeAt 9t s =, system parameters are abruptly changed to 15P =,35R =, and 12/3b =. Accordingly the new equilibrium is changedto 2121(,,)(8.5,8.5,18.1)T Tr r r x x x b =. Obviously, aftervery short transient duration, system state converges to the new point, as shown in Fig.3(a). Fig.4(a) represents the evolution in time of the L yapunov function.B. Simulation results in the presence of set pointchangeAt 9t s =, the target is abruptly changedto 2121(,,)(12,12,54)T Tr r r x x x b =, then the responsesof the system state are shown in Fig.3(b). In Fig.4(b) the time history of the L yapunov function is expressed.t/sx 1,x 2,x 3t/sx 1,x 2,x 3Fig.3. State responses (a) in the presence of parameter variations, (b) in the presence of set point changet/sL y a p u n o v f u n c t i o n Vt/sL y a p u n o v f u n c t i o n VFig.4. Time history of the Lyapunov fu nction (a) in the presence of parameter variations, (b) in the presence of set point changeC. Simulation results in the presence ofdisturbanceIn Eq.(5)external periodic disturbance3cos(5),1,2,3i w t i π==is considered. The time responses of the system states are given in Fig.5. After control the steady-state phase plane trajectory describes a limit cycle, as shown in Fig.6.t/sx 1,x 2,x 3Fig.5. State responses in the presence of periodic disturbancex1x 3Fig.6. The state space trajectory at [10,12]t ∈in the presence ofperiodic disturbanceD. Simulation results in the presence of randomnoiseUnder the influence of random noise,112121132231233xPx Px x Rx x x x u xx x bx εδεδεδ=-++⎧⎪=--++⎨⎪=-+⎩ (51) where ,1,2,3i i δ= are normally distributed withmean value 0 and variance 0.5, and 5ε=. The results of the numerical simulation are depicted in Fig.7,which show that the steady responses are hardly affected by the perturbations.t/sx 1,x 2,x 3t/se 1,e 2,e 3Fig.7. Time responses in the presence of random noise (a) state responses, (b) state tracking error responses4.2 Simulation results of control the trajectory to periodic orbitIf the reference signal is periodic, then the system output will also track this signal. Figs.8(a) to (d) show time responses of 1()x t and the tracking trajectories for 3-Period and 4-period respectively.t/sx 1x1x 2t/sx 1x1x 2Fig.8. State responses and the tracking periodic orbits (a)&( b)3-period, (c)&(d) 4-periodRemark 3 The two controllers designed above solved the chaos control problems of Lorenz chaoticsystem, and the controller design method can also beextended to solve the chaos suppression problems of the whole Lorenz system family, namely the unified chaotic system.[44-46] The detail design process and close-loop system analysis can reference to the author ’s another paper.[47] In Ref.[47] according to different positions the scalar control input added,three controllers are designed to reject the chaotic behaviors of the unified chaotic system. Taking the first state 1x as the system output, by transforming system equation into the normal form firstly, the relative degree r (3r ≤) of the controlled systems i s known. Then we can design the controller with the expression as Eq.(3) and Eq.(4). Three effective adaptive nonlinear compensating mechanisms are derived to compensate the chaotic system nonlinearities and external disturbances. According toL yapunov stability theory sufficient conditions for the choice of control parameters are deduced so that designers can tune the design parameters in an explicit way to obtain the required closed loop behavior. By numeric simulation, it has been shown that the designed three controllers can successfully regulate the chaotic motion of the whole family of the system to a given point or make the output state to track a given bounded signal with great robustness.5. ConclusionsIn this letter we introduce a promising tool to design control system for chaotic system subject to persistent disturbances, whose entire dynamics is assumed unknown and the state variables are not completely measurable. By integral action the nonlinearities, including system structure nonlinearity, various disturbances, are compensated successfully. It can handle, therefore, a large class of chaotic systems, which satisfy four assumptions. Taking chaotic Lorenz system as an example, it has been shown that the designed control scheme is robust in the sense that the unmeasured states, parameter uncertainties and external disturbance effects are all compensated and chaos suppression is achieved. Some advantages of this control strategy can be summarized as follows: (1) It is not limited to stabilizing the embeddedperiodic orbits and can be any desired set points and multiperiodic orbits even when the desired trajectories are not located on the embedded orbits of the chaotic system.(2) The existence of parameter uncertainty andexternal disturbance are allowed. The controller can be designed according to the nominal system.(3) The dynamic characteristics of the controlledsystems are approximately linear and the transient responses can be regulated by the designer through controllerparameters ,0,,1i h i r =- .(4) From L yapunov stability theory sufficientconditions for the choice of control parameters can be derived easily.(5) The error converging speed is very fast evenwhen the initial state is far from the target one without waiting for the actual state to reach the neighborhood of the target state.AppendixSimulation results of control scheme 1.t/sx 1,x 2,x 3t/sL y a p u n o v f u n c t i o n VFig.A1. (a) State responses u nder control, (b) Time history of the Lyapunov functiont/sx 1,x 2,x 3t/sx 1,x 2,x 3Fig.A2. State responses (a) in the presence of parameter variations, (b) in the presence of set point changet/sL y a p u n o v f u n c t i o n Vt/sL y a p u n o v f u n c t i o n VFig.A3. Time history of the L yapu nov fu nction (a) in the presence of parameter variations, (b) in the presence of set point changet/sx 1,x 2,x 3Fig.A4. State responses in the presence of periodic disturbanceresponsest/sx 1,x 2,x 3Fig.A5. State responses in the presence of rand om noiset/sx 1x1x 2Fig.A6. State response and the tracking periodic orbits (4-period)References[1] Lü J H, Zhou T S, Zhang S C 2002 C haos Solitons Fractals 14 529[2] Yoshihiko Nagai, Hua X D, Lai Y C 2002 C haos Solitons Fractals 14 643[3] Li R H, Xu W , Li S 2007 C hin.phys.16 1591 [4]Xiao Y Z, Xu W 2007 C hin.phys.16 1597[5] Ott E ,Greb ogi C and Yorke J A 1990 Phys.Rev .Lett. 64 1196 [6]Yoshihiko Nagai, Hua X D, Lai Y C 1996 Phys.Rev.E 54 1190 [7] K.Pyragas, 1992 Phys. Lett. A 170 421 [8] Lima,R and Pettini,M 1990 Phys.Rev.A 41 726[9] Zhou Y F, Tse C K, Qiu S S and Chen J N 2005 C hin.phys. 14 0061[10] G .Cicog na, L.Fronzoni 1993 Phys.Rew .E 30 709 [11] Rakasekar,S. 1993 Pramana-J.Phys.41 295 [12] Gong L H 2005 Acta Phys.Sin.54 3502 (in C hinese) [13] Chen L,Wang D S 2007 Acta Phys.Sin.56 0091 (in C hinese) [14] C hen G R and Dong X N 1993 IEEE Trans.on Circuits andSystem-Ⅰ:Fundamental Theory and Applications 40 9 [15] J.L. Kuang, P.A. Meehan, A.Y.T. Leung 2006 C haos SolitonsFractals 27 1408[16] Li R H, Xu W, Li S 2006 Acta Phys.Sin.55 0598 (in C hinese) [17] Yu X 1996 Int.J.of Systems Science 27 355[18] Hsun-Heng Tsai, C hyu n-C hau Fuh and Chiang-Nan Chang2002 C haos,Solitons Fractals 14 627[19] Her-Terng Yau and C hieh-Li C hen 2006 C hao ,SolitonsFractal 30 709[20] Guo H J, Liu J H, 2004 Acta Phys.Sin.53 4080 (in C hinese) [21] Yu D C, Wu A G , Yang C P 2005 Chin.phys.14 0914 [22] C hyu n-C hau Fuh and Pi-Cheng Tu ng 1995 Phys.Rev .Lett.752952[23] Chen L Q, Liu Y Z 1998 Applied Math.Mech. 19 63[24] Liu D, R en H P, Kong Z Q 2003 Acta Phys.Sin.52 0531 (inChinese)[25] Liu H, Liu D and Ren H P 2005 Acta Phys.Sin.54 4019 (inChinese)[26] C hang W , Park JB, Joo YH, C hen GR 2002 Inform Sci 151227[27] Gao X, Liu X W 2007 Acta Phys.Sin. 56 0084 (in C hinese) [28] Chen S H, Liu J, Lu J 2002 C hin.phys.10 233 [29] Lu J H, Zhang S. 2001 Phys. Lett. A 286 145[30] Liu J, Chen S H, Xie J. 2003 C haos Solitons Fractals 15 643 [31] Wang J, Wang J, Li H Y 2005 C haos Solitons Fractals 251057[32] Wu X Q, Lu JA, C hi K. Tse, Wang J J, Liu J 2007 ChaoSolitons Fractals 31 631[33] A.L.Fradkov , R .J.Evans, 2002 Preprints of 15th IF AC W orldCongress on Automatic Control 143[34] Zhang H G 2003 C ontrol theory of chaotic systems (Shenyang:Northeastern University) P38 (in C hinese)[35] Yu-Chu Tian, Moses O.Tadé, David Levy 2002Phys.Lett.A.296 87[36] Jose A R , Gilberto E P, Hector P, 2003 Phys. Lett. A 316 196 [37] Liao X X, Yu P 2006 Chaos Solitons Fractals 29 91[38] Tornambe A, V aligi P.A 1994 Measurement, and C ontrol 116293[39] Andrew Y.T.Leung, Liu Z R 2004 Int.J.Bifurc.C haos 14 2955 [40] Qu Z L, Hu,G .,Yang,G J, Qin,G R 1995 Phys.Rev .Lett.74 1736 [41] Y ang J Z, Qu Z L, Hu G 1996 Phys.Rev.E.53 4402[42] Shyi-Kae Yang, C hieh-Li Chen, Her-Terng Yau 2002 C haosSolitons Fractals 13 767。

2023北京丰台初三(上)期中英语(教师版)

2023北京丰台初三(上)期中英语(教师版)

2023北京丰台初三(上)期中英语2023.11第一部分本部分共33题,共40分。

在每题列出的四个选项中,选出最符合题目要求的一项。

一、单项填空(每题0.5分,共6分)从下面各题所给的A、B、C、D四个选项中,选择可以填入空白处的最佳选项。

1. Jack is very kind. He often helps ____with my English.A. meB. mineC. ID. my2. My father was born__1980.A. atB. inC. onD. to3. I can look after myself, ___ it won’t be easy for me.A. becauseB. orC.soD. although4. —________ do you play basketball? —Once a week.A. How oftenB. How longC. How muchD. How far5. Bill does sports every day. He is one of ________ boys in my class.A. strongB. strongerC. strongestD. the strongest6. — Can you ride a bike?—No, I________.A. needn’tB. can’tC. may notD. mustn’t7. Mike and I ________ football yesterday. We had a good time.A. playB. will playC. playedD. are playing8. Where’s Helen? Her mother ________ her now.A. is looking forB. will look forC. has looked forD. looks for9. My uncle is a song writer. He ________ more than twenty songs since 2018.A. writesB. wroteC. has writtenD. will write10. —What were you doing at this time yesterday?—I ________ in the park.A. walkB. walkedC.am walkingD. was walking11. If you listen carefully in class, you________ what to do.A. understandB. understoodC. will understandD. have understood12. —Do you know ________ tomorrow?—At 9 o’clock in the morning.A. when will Mary comeB. when Mary will comeC. how will Mary comeD. how Mary will come二、完形填空(每题1分,共8分)阅读下面的短文,掌握其大意,然后从短文后各题所给的A、B、C、D四个选项中,选择最佳选项。

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M.-J. Wang & X.-Y. Wang
Fig. 1.
The chaotic attractor of Liu system.
Fig. 2.
The projections of Liu attractor.
2. Description of Liu System Liu system15 is described as ˙ = a(y − x) x y ˙ = bx − kxz . z ˙ = −cz + hx2
1. Introduction In 1990, Ott, Grebogi and Yorke presented the OGY method to control chaos.1 After their pioneering work, chaotic control has become a focus in nonlinear problems and a lot of work has been done in the field.2 – 4 Nowadays, many methods have been proposed to control chaos.5,6 Generally speaking, there are two kinds of control ways: feedback control and nonfeedback control. Feedback methods7 – 11 are used to stabilize the unstable periodic orbit of chaotic systems by feeding back their states. Nonfeedback methods11 – 14 are adopted to change chaotic behaviors by applying perturbations to some parameters or variables. In this paper, we use these two methods to control the dynamic behavior of Liu system. With the direct feedback method, Liu system can be stabilized at equilibrium point or limit cycle around its equilibrium. With the adaptive time-delayed feedback method, Liu system can be stabilized at its original unstable periodic orbit. In the nonfeedback method, periodic parametric perturbation with different frequencies can control Liu system to not only periodic motion but also hyperchaos. Numerical simulations show the effectiveness of these methods.
(1)
When a = 10, b = 40, c = 2.5, h = 4 and k = 1, system (1) exhibits a chaotic behavior. Its attractor is shown in Fig. 1. The projections of system (1)’s attractor are shown in Fig. 2. In fact, Liu system is closely related to the generalized Lorenz system family. Next, some results in the existing references will be cited to clarify this point. The following nonlinear system of ordinary differential equations is called the generalized Lorenz system (GLS):16 0 0 0 A 0 a11 a12 x ˙ = z + x1 0 0 −1 x, , (2) A= a21 a22 0 λ3 0 1 0 where x = [x1 , x2 , x3 ]T , λ3 ∈ R, and A has eigenvalues λ1 , λ2 ∈ R, λ1 > 0, λ2,3 < 0. This GLS is said to be nontrivial if it has at least one solution that goes neither to zero nor to infinity nor to a limit cycle.
The following results, clarifying the relation between GLS and GLCF, were presented in Ref. 17: For the nontrivial GLS (2), there exists a nonsingular oneparameter linear transformation of coordinates, z = Tτ x, which takes GLS (2) into GLCF (3) with τ > −1. Liu system has been proven to be a special case of the proposed generalized Lorenz system family.21 Actually, GLCF (3) with τ = −1 is equivalent to Liu system according to Ref. 21. Via the following linear transformation of coordinates, √ x = x√ hk (5) y = y hk , z = kz system (1) with a, b, c, k, h > 0 is equivalent to ˙ x = a(y − x ) ˙ = bx − x z . y ˙ z = −cz + x 2
Modern Physics Letters B, Vol. 23, No. 14 (2009) 1805–1818 c World Scientific Publishing Company
CONTROLLING LIU SYSTEM WITH DIFFERENT METHODS
MINGJUN WANG∗ and XINGYUAN WANG† School of Electronic & Information Engineering, Dalian University of Technology, Dalian 116024, China ∗ wmjhome@ † wangxy@ Received 31 August 2008 Revised 10 September 2008 In this paper, two different kinds of methods are adopted to control Liu system — feedback method and nonfeedback method. On the one hand, direct feedback and adaptive time-delayed feedback are taken as examples for the study of feedback control. In the direct feedback method, Liu system can be stabilized at one equilibrium point or a limit cycle surrounding its equilibrium. In the adaptive time-delayed feedback method, feedback coefficient and delay time can be adjusted adaptively to stabilize Liu system at its original unstable periodic orbit. On the other hand, periodic parametric perturbation is used to control chaos in Liu system as a typical nonfeedback method. By changing the frequency of the perturbation signal, Liu system can be guided to not only periodic motion but also hyperchaos. Numerical simulations show the effectiveness of our methods. Keywords : Liu system; chaotic control; equilibrium point; limit cycle; hyperchaos.
(6)
In the same way, for any λ1 , λ2 , λ3 ∈ R, λ1 > 0, λ2,3 < 0, GLCF (3) with τ = −1 is equivalent to Eq. (6) via λ2 − λ1 x = (z1 − z2 ) λ2 + λ1 λ2 − λ1 λ2 z1 − λ1 z2 (7) y = λ + λ λ + λ 2 1 2 1 z = z3 λ2 − λ1 λ2 + λ1
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