SIR-20 用户手册 REV.A
1-SIR-20操作手册解析
SIR-20 操作手册美国劳雷工业有限公司第一章介绍 (1)1.1仪器系统 (1)第二章二维测量参数设置 (1)2.1: System Parameter Setup 系统参数设置 (1)Create Folders 创建文件夹 (2)Set Program Defaults 设置缺省值 (2)Set working directories 设置工作目录 (3)2.2: Setting Up your System for 2D Data Collection 二维测量 (4)Projects and Profiles: How the SIR-20 Collects Data 项目 (4)The File Header 文件头 (4)Collection Parameters 采集参数设置 (5)2.3: Data Collection Methods 数据采集方法 (7)Survey Wheel Controlled Collection 测量轮控制测量 (7)Position/Range信号位置/时间窗口 (14)Gain增益 (15)Filters and Stacking滤波和叠加 (17)During Collection 数据采集 (18)Time-Based (Free run continuous) Data Collection 连续测量数据采集 (18)Point Mode Data Collection 点测 (19)附录D:装好的SIR-20配置 (1)第一章介绍本手册适用于地质雷达新老用户。
无论你是否具有地质雷达的使用经验,都建议你完整地阅读本手册,并且参考附录F中的相关书籍。
1.1仪器系统SIR-20系统预装了操作系统和采集处理软件。
如果单独购买SIR-20,则SIR-20系统包含以下部件:数字控制单元MF-20:蓝色矩形盒,一侧带有电风扇和后面是各种接口。
ToughBook 光驱。
IWN A2410(Rev.A)用户手册
IWN A2410(Rev.A)无线接入点(AP)用户手册西安西电捷通无线网络通信有限公司商标、版权声明如果未经书面许可,用户不得打开设备机壳或对本设备进行任何改造。
商标、版权声明IWNCOMM 及AirSec为西安西电捷通无线网络通信有限公司商标。
本产品的所有部分,包括配件和软件,其版权都为西安西电捷通无线网络通信有限公司所有,未经任何事先书面授权,不得任意仿制,拷贝,抄写或转译。
如内容更新,恕不另行通知,可随时查阅我们的网页 版权所有 不得翻印AirSec IWN A2410(Rev.A)用户手册手册说明感谢您选购捷通通信AirSec系列企业级无线局域网产品——IWN A2410(Rev.A)室内无线接入点,本手册将指导您完成无线接入点的安装和配置等工作。
本产品应包含以附件● IWN A2410室内无线接入点(1台)● 天线(2支)● 12VDC电源适配器(1台)● 电源线(1根)● 产品合格证/保修卡● 用户手册电子档光盘注意:如果有任何的东西遗失,请向原购买厂商索取捷通通信声明本设备属于低功率的无线发射和接收装置,开机后,它发射低等级无线电能(又称无线电波或无线电频场)不会对人体产生任何伤害。
但用户安装或使用不当,可能会对其它无线电通信等设备造成一定的干扰,所以,请您遵照手册内安装说明书。
如果未经书面许可,用户不得打开设备机壳或对本设备进行任何改造。
目录商标、版权声明 01 简介 (1)2 设备安装 (2)2.1产品信息 (2)2.2系统安装要求 (2)2.3硬件安装 (2)2.3.1 选址 (2)2.3.2 连接以太网电缆 (2)2.3.3 连接电源 (3)3配置 (4)3.1登录WEB管理 (4)3.2系统登录 (8)3.3基本配置: (11)3.4系统配置 (12)3.4.1系统状态 (12)3.4.2更改帐户 (13)3.4.3系统重启动 (15)3.4.4恢复默认配置 (17)3.4.5 数据备份 (19)3.4.6 数据恢复 (21)3.5系统功能配置 (24)3.5.1MAC地址过滤 (24)3.5.2无线参数配置 (26)3.6WAPI配置 (27)3.6.1本地AS管理 (27)3.6.1.1 AS配置 (28)3.6.1.2 证书分发 (28)3.6.1.3 证书查询 (32)3.6.2 认证加密配置 (34)3.6.2.1 名词解释 (34)3.6.2.2 启用共享密钥安全机制 (36)3.6.2.3 启用证书安全机制 (36)3.7退出系统 (40)3.8硬件恢复默认设置 (40)1 简介完全符合“中国无线局域网国家标准GB15629.11/1102/1104”的AirSec系列产品,结合优异的性能与良好的向下兼容性,最大限度地保护了用户的投资,向无线网络界展现了一整套全新的无线网络宽频接入方案。
设备数据通知用户手册 M00084500 Rev.A说明书
Device Data NotificationUser’s ManualOverviewDescribes the operating environment and system config-uration for Device Data Notification.Sample ProgramDescribes how to use the sample program and how toconfigure the system.Request and ResponseDescribes the requests and responses in Device DataNotification.M00084500Rev.ACautions•No part of this document may be reproduced, stored in a retrieval system, or transmitted in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of Seiko Epson Corporation.•The contents of this document are subject to change without notice. Please contact us for the latest information.•While every precaution has taken in the preparation of this document, Seiko Epson Corporation assumes no responsibility for errors or omissions.•Neither is any liability assumed for damages resulting from the use of the information contained herein.•Neither Seiko Epson Corporation nor its affiliates shall be liable to the purchaser of this product or third parties for damages, losses, costs, or expenses incurred by the purchaser or third parties as a result of: accident, misuse, or abuse of this product or unauthorized modifications, repairs, or alterations to this product, or (excluding the U.S.) failure to strictly comply with Seiko Epson Corporation’s operating and maintenance instructions.•Seiko Epson Corporation shall not be liable against any damages or problems arising from the use of any options or any consumable products other than those designated as Original EPSON Products or EPSON Approved Products by Seiko Epson Corporation.TrademarksEPSON is a registered trademark of Seiko Epson Corporation.Exceed Your Vision is a registered trademark or trademark of Seiko Epson Corporation.Windows® and Internet Explorer® are either registered trademarks or trademarks of Microsoft Corporation in the United States and other countries.All other trademarks are the property of their respective owners and used for identification purpose only.© Seiko Epson Corporation 2014. All rights reserved.2For SafetyThe symbols in this manual are identified by their level of importance, as defined below. Read the following carefully before handling the product.Restriction of UseWhen this product is used for applications requiring high reliability/safety such as transportation devices related to aviation, rail, marine, automotive etc.; disaster prevention devices; various safety devices etc; or functional/precision devices etc, you should use this product only after giving consideration to including fail-safes and redundancies into your design to maintain safety and total system reliability. Because this product was not intended for use in applications requiring extremely high reliability/safety such as aerospaceequipment, main communication equipment, nuclear power control equipment, or medical equipment related to direct medical care etc, please make your own judgment on this product’s suitability after a full evaluation.3About this ManualThis manual presents information that is necessary information for using the TM-Intelligent.The TM-Intelligent series in this manual is a generic term for the TM-i series.The TM-i series in this manual is a generic term for the following printers.∙TM-T88V-i∙TM-T70-i∙TM-T20II-i∙TM-T82II-i∙TM-T83II-iThe manual is made up of the following sections:Chapter 1OverviewChapter 2Sample ProgramChapter 3Request and Response4Contents■For Safety (3)Key to Symbols (3)■Restriction of Use (3)■About this Manual (4)Aim of the Manual (4)Manual Content (4)■Contents (5)Overview (7)■Overview of Device Data Notification (7)■Operating Environment (8)How to Access the Web server (8)TM Intelligent Printer (8)Input Device (8)Control Device (9)■Contents In the Package (10)Manual (10)Sample Program (10)Download (10)Sample Program (11)■Overview (11)Hardware Configuration (11)File Configuration (12)Printing Result (12)Program Flow (13)■Environment Settings (14)Sample Program Configuration (15)TM Intelligent Printer Settings (16)■Execution of Sample Program (18)5Request and Response (19)■Request (Device Use Rights Acquisition Result Notification) (19)■Response (Device Use Rights Acquisition Result Notification) (20)■Request (Input Data from Input Device) (21)■Response (Input Data from Input Device) (22)■Request (Device Control Execution Result) (23)■Response (Device Control Execution Result) (24)■Response to Disable Device Control (24)67Chapter 1 Overview 1This chapter provides the overview of Device Data Notification.Overview of Device Data NotificationDevice Data Notification is a function used to post the data input from the input device that is connected to the TM intelligent printer to the designated URL of the Web server. The Web server application performs device control, such as printing and displaying information on the customer display, by including print data in ePOS-Device XML format and device control into the response to a request from the TM intelligent printer.1 : When a data input occurs, for example, when an operator reads a barcode with the barcode reader,the input device sends the input data to the TM intelligent printer.2 : The TM intelligent printer formats the input data received from the input device and sends the data tothe Web server application (POST).3 : Triggered by the input data, the Web server application generates device control data in ePOS-DeviceXML format from database or other system and returns a response to the request from the TM intelligent printer.4 : The TM intelligent printer sends the device control data to the device.5 : The TM intelligent printer sends the result of device control to the Web server.Web server8Operating Environment ❏TM-T88V-i (TM-i firmware Ver.4.1 or later)❏TM-T70-i (TM-i firmware Ver.4.1 or later)❏TM-T20II-i (TM-i firmware Ver.4.1 or later)❏TM-T82II-i (TM-i firmware Ver.4.1 or later)❏TM-T83II-i (TM-i firmware Ver.4.1 or later)Input DeviceThe following devices can be designated as the input device for Device Data Notification:❏Key input device (keyboard, barcode scanner, etc.)❏Serial communication device❏Communication box in the TM intelligent printer Proxy server✔Proxy authentication✔Digest authentication✔HTTPS communication✔HTTPS communication with server authentication ✔9Chapter 1 Overview 1The following devices can be designated as the control device for Device Data Notification:❏Main printer of the TM intelligent printer❏TM printer *❏Customer display❏Serial communication device❏Communication box in the TM intelligent printer* : Available TM printers are different depending on the TM-i Firmware version in the TM intelligent printer. For details, refer to Technical Reference Guide for each printer.The device designated as the input device or control device is locked with exclusive lock byDevice Data Notification. Therefore, the designated device cannot be controlled by ePOS-Device SDK or ePOS-Device XML.Contents In the Package❏Device Data Notification User's Manual (This Document)❏Technical Reference Guide for each printer❏ePOS-Device XML User's manualDDN_Sample_Vxxx.zip Sample program for Device Data Notification Test_DeviceData.php Sample program fileREADME.txt Readme fileFor customers in North America, go to the following web site:/ and follow the on-screen instructions.For customers in other countries, go to the following web site:https:///?service=pos10Chapter 2 Sample ProgramThis chapter describes how to use the sample program for Device Data Notification.OverviewThe sample program that uses PHP can be registered to the Web server and be operated.When a barcode is read with the scanner, the TM intelligent printer sends a request containing barcode data to the sample program in the Web server. The sample program sends response data containing print data in ePOS-Device format and display data. The main printer of the TM intelligent printer prints a coupon and displays a message on the customer display.❏TM Intelligent Printer❏Scanner❏Customer display (Use of the customer display is optional.)Test_DeviceData.php The server returns a response containing print data when the printer sends a request.Chapter 2 Sample Program 2The flow from the initial display to the print completion of the sample program is as shown below.3. Returning the print data/customer display data to the printer2. Sending the data read with the scanner to the Web server1. Reading a barcode with the scanner4. Printing the data and displaying a message on the customer display5. Sending the print result/customer display result to the Web serverEnvironment SettingsThe environment setting flow of the sample program is as shown below.1. Router SettingsSet information such as SSID, IP address, DHCP and allocated IP address. For details, seethe manual for each device.2. Web Server Settings1. Web Server ConfigurationConfigure IIS and XAMPP in the computer.2. Sample Program Configuration (p.15)Save the sample program files in the computer.3. Network SettingsConfigure the network settings such as IP address to the computer.3. TM Printer Network SettingsConfigure the network settings such as IP address to the TM printer to be connected.Configure the network settings such as IP address to the printer by using EPSON TMNetWebConfig from a Web browser on the setup computer.For the configuration procedure, refer to the Technical Reference Guide for each TMprinter.Chapter 2 Sample Program 2Save the sample program files to the Web server.Save the files directly under the following folders:IISinetpub\wwwroot Test_print.phpXAMPP xampp\htdocs 4. TM Intelligent Printer Settings (p.16)1. IP Address SettingSet the IP address.For details on how to set, refer to Technical Reference Guide for each printer.4. Device Data Notification Settings (p.17)Configure the Device Data Notification settings.3. Register the Devices (p.16)Register the scanner and customer display .2. Register the TM PrintersRegister the TM printer to be used for printing. Not required for the sample program.Register the DevicesRegister the scanner and customer display using EPSON TMNet WebConfig.1Turn off the TM intelligent printer and connect the scanner and customer display . Then, turn on the TM intelligent printer.2Start the Web browser on the setup computer and enter as follows:http://[IP address of the TM -i ]/webconfig/3EPSON TMNet WebConfig starts.4Register the scanner.Select [configuration] - [Web Service Settings] - [Device Admin] - [Device Registration] - [Key Input Device]. 5The “Key Input Device” screen appears.Set the following items and click [Apply].6The scanner is added to the registered key input devices. Click [Operating test] and check whether the registered scanner operates properly .7Register the customer display .Select [configuration] - [Web Service Settings] - [Device Admin] - [Device Registration] - [Customer Display]. 8The "Customer Display" screen appears. Set the following items and click [Apply].Device IDSet the device ID. Enter "local_scanner".Device nameConfirm that the connected scanner is selected.Control script Set the control script. Select "Scanner_Generic.js".Customer DisplaySelect [Use].Communicationsettings Communicationspeed (bps)Set the communication speed.Select the communication speed according to the customer display .Data bitSet the data bit.Select the data bit according to the customer display .ParitySet the parity .Select the parity according to the customer display .Brightness setting Set the brightness. Select the brightness as desired.Chapter 2 Sample Program 29The customer display is registered.Click [Test display] and check whether the registered customer display operatesproperly .Device Data Notification SettingsConfigure the Device Data Notification settings using EPSON TMNet WebConfig as follows:1EPSON TMNet WebConfig starts.Select [configuration] - [Web Service Settings] - [Server Access] - [Device Data Notification].2The "Device Data Notification" screen appears. Set the following items and click[Apply].ItemDescription settingsDevice Data NotificationSelect [Enable].Server AccessID Set this item to use HTTP digest authentication or to identify the main printer from the server.Not required for the sample program.Password Set this item to use HTTP digest authentication.Not required for the sample program.URLEnter the URL of the Device Data Notification destination(sample program). Enter as follows:http://[IP address of the Web server]/Test_DeviceData.php After entry, check whether the URL is correct. Click [Access Test].ServerAuthentication Set this item to perform server authentication with the registered certificate during access with https.Not required for the sample program.Box ID Specify the box ID of the communication box to becontrolled by the Device Data Notification function.To use the communication box by the Device DataNotification function, set the member ID for sending data tothe communication box as ""(null).Not required for the sample program.POST Error Print MessageTo print an error message when POST to the server fails, select [Enable].Message Text Enter the character string to be printed when POST to theserver fails.Text AttributesSet the character decoration for message. Select thecharacter decoration to be used. The following decorationsare available:Bold /Underline /Double width /Double height /Reverseblack and white /Upside downCut To cut the paper after printing an error message, select[Enable].Execution of Sample Program1Confirm that Device Data Notification is enabled using EPSON TMNet WebConfig.2Read a barcode using the scanner connected to the TM intelligent printer.3To the request from the TM intelligent printer, print data is returned as a responseand a coupon is printed from the printer. A message is displayed on the customerdisplay .Capture DeviceDeviceSelect the device to be used.For the sample program, select the following items:∙local_printer∙local_display∙local_scannerChapter 3 Request and Response 3This chapter describes data inputs from the input device, requests from the TM intelligent printer, andresponses from the Web server.Request (Device Use Rights Acquisition Result Notification)When the TM intelligent printer is turned on, or when the Device Data Notification settings are changed with EPSON TMNet WebConfig, the TM intelligent printer executes <open_device> in ePOS-Device XML toenable the device designated as the input/control device, formats the result in ePOS-Device XML format, and sends a HTTP POST request as shown below.The format of request message is URL-encoded form data (application/x-www-form-urlencoded). Set the sending destination according to "Device Data Notification" (p. 17).TM intelligent printer sends one HTTP request (Device Use Rights Acquisition Result Notification) to the Web server for each device. Therefore, when multiple devices are set as the target device for Device DataNotification, multiple HTTP requests (Device Use Rights Acquisition Result Notification) are sent to the Web server.ParameterValue IDThe ID set with WebConfig (p. 17)DataePOS-Device XML formatPOST /Test_DeviceData.php HTTP/1.1Host: 192.168.192.10Content-Type: application/x-www-form-urlencodedContent-Length: xxxID=&Data=<open_device><device_id>local_printer</device_id><code>OK</code><data_id>1</data_id></open_device>HeaderResponse (Device Use Rights Acquisition Result Notification)The Web server application creates response data as shown below to a HTTP request (Device Use Rights Acquisition Result Notification) and returns it to the TM intelligent printer. This data contains device control data.The format of response message is ePOS-Device XML(text/xml).When no device control is required, refer to "Response to Disable Device Control" (p.24).HTTP/1.1 200 OKContent-Type: text/xml; charset=utf-8Content-Length: xxx<device_data><device_id>local_keyboard</device_id><data><type>setprefix</type>..</data></device_data>\0* For the <device_data> tag, be sure to end the message with "\0".Chapter 3 Request and Response3Request (Input Data from Input Device)When data is input from the input device, the TM intelligent printer formats the input data received from the input device in ePOS-Device XML format and sends a HTTP POST request as shown below to the Web server.The format of request message is URL-encoded form data (application/x-www-form-urlencoded). Set the sending destination according to "Device Data Notification" (p. 17).ParameterValueID The ID set with WebConfig (p. 17)DataePOS-Device XML formatPOST /Test_DeviceData.php HTTP/1.1Host: 192.168.192.10Content-Type: application/x-www-form-urlencoded Content-Length: xxxID=&Data=<device_data><sequence>0</sequence><device_id>local_scanner</device_id><data><input>XXXXXX</input><type>ondata</type></data><data_id>X</data_id></device_data>HeaderResponse (Input Data from Input Device)The Web server application creates response data as shown below to a HTTP request (Input Data) and returns it to the TM intelligent printer. This data contains device control data.The format of response message is ePOS-Device XML(text/xml).When no device control is required, refer to "Response to Disable Device Control" (p.24).HTTP/1.1 200 OKContent-Type: text/xml; charset=utf-8Content-Length: xxx<device_data><device_id>local_keyboard</device_id> <data><type>print</type><Timeout>10000</Timeout> <printdata><epos-print xmlns="/schemas/2011/03/epos-print">..</epos-print> </printdata> </data></device_data>\0<device_data><device_id>local_display</device_id> <data><type>display</type><Timeout>10000</Timeout> <displaydata><epos-print xmlns="/schemas/2011/03/epos-print">..</epos-print> </displaydata> </data></device_data>\0* For the <device_data> tag, be sure to end the message with "\0".Chapter 3 Request and Response3Request (Device Control Execution Result)received from the Web server, formats the result in ePOS-Device XML format, and sends a HTTP POST request as shown below.The format of request message is URL-encoded form data (application/x-www-form-urlencoded). Set the sending destination according to "Device Data Notification" (p. 17).When the TM intelligent printer receives multiple device control data items from the Web server, the TM intelligent printer executes each device control result separately . The device control execution result is sent as one HTTP request (Device Control Execution Result) to the Web server for each device control.ParameterValueID The ID set with WebConfig (p. 17)DataePOS-Device XML formatPOST /Test_DeviceData.php HTTP/1.1Host: 192.168.192.10Content-Type: application/x-www-form-urlencoded Content-Length: xxxID=&Data=<device_data><sequence>0</sequence><device_id>local_scanner</device_id><data><resultdata><response success=”true” code=”” status=”251658262” battery=”0” xmlns=”/schemas/2011/03/epos-print”/></resultdata><type>onxmlresult</type></data><data_id>5</data_id></device_data>HeaderResponse (Device Control Execution Result)returns it to the TM intelligent printer. For the responses, refer to "Response to Disable Device Control" (p.24). Response to Disable Device ControlWhen no device control is required, notifies that there is no device control data by returning the response as shown below to a HTTP request from the TM intelligent printer.Refer to Test_DeviceData.php in the sample program.HTTP/1.1 200 OKContent-Type: text/xml; charset=utf-8Content-Length: 0。
SIR-20 用户手册
第一部分:启动和基本项目的安装SIRveyor SIR 20 是有2 个硬件道(天线),4个记录道的高性能地质雷达(GPR)系统。
SIRveyor被用来记录、处理和显示地下特征的剖面和三维图象(如果有三维格式采集的资料)。
该系统配有标准的GSSI天线,能被用于各种应用领域,来解决复杂的地下探测问题和构造探测问题。
SIRveyor允许我们:●采集:由一个天线采集到4道的数据由两个天线采集到4道的数据二维格式的单一剖面三维格式数据的采集●野外处理数据●复查和显示二维剖面或三维格式的野外数据,1.1 系统启动1、把选择的电源连接到SIRveyor SIR-20设备上(当只有掌上电脑电池时系统不运行)2、接通计算机;开关位于以太网连接器后边计算机右部的后面。
3、一旦计算机接通,并且SIR-20已插入,则系统就运行。
4、过几分钟,显示器灯将闪两下,然后就保持稳定了。
更多的信息请查附录B。
1.2 软件和新项目设置先打开RADAN系统信息屏幕,就可找到软件版本和序列号。
该屏幕将在30秒后消失,或点击鼠标左键跳到下一屏幕。
为了采集数据,特别设置了SIRveyor 的快捷键。
虽然RADAN软件屏幕和SIRveyor 的屏幕好象相同,但两者的配置是不同的,因而数据不能通过RADAN 快捷键采集。
目录、长度和数据库的系统设置这些命令使你能安装系统,以便在新地区收集数据。
如果你希望继续做先前的项目,就跳到1.4部分打开存在的项目文件。
否则,就按以下步骤进行。
第一步是设置数据目录。
对每个工区或每项工作创建新的数据目录,会使管理数据更容易。
应该先指定一个单独的输出目录路径,以便让软件将已处理的数据放到该输出目录。
1、设置文件信息选择视窗>Customize(用户自选)。
2、选择目录表,然后设置源目录和输出目录。
注释:Customize ——用户自选Directories ——目录Appearance ——状态,外观Database ——数据库Linear Units ——长度Source ——源目录Output ——输出目录OK——确定Cancel——取消Apply——应用Help ——帮助3、选择长度列表,然后设置想要的单位。
Microsoft Word - Sir20探地雷达doc
于硬盘容量的大小。
技术参数 : 增益范围:-20—+100 dB 可。增益曲线分段可以从 1—8 进行选择。
垂直滤波:时间域滤波。无限脉冲影响(IIR)、有限脉冲影像(FIR)、矩形和三角形高低 通滤波器。 IIR: 低通: 双级; 高通:双级 FIR,矩形和三角形 低通: 最多 1/2 扫描长度; 高通: 最多 1/2 扫描长度 水平滤波: IIR: 叠加:1—16384 个扫描; 背景消除:1—16384 个扫描 静态: 叠加:2—32768 个扫描; 雷达系统连接: 双天线输入;1 个 12 V 直流电源输入;1 个测量轮或测距输入器;1 个里程输入 物理特性: 尺寸:466 mm x 395 mm x 174 mm (18.4 x 15.5 x 6 in) 重量:10 kg (22 lbs) 电子元件: 天线:所有的 GSSI 模式天线都可使用,并且能够同时配接 2 个天线。 分辨率:5 ps 范围:0—8,000 ns,可选 数据输出格式:8 位或 16 位可选 扫描样点数:256,512,1024,2048,可选 扫描速率:2—800 次/秒,可选 输入电源:12V 直流(11—15V 范围内),60W 温度: 工作温度:-10℃—40℃;相对湿度:<95%(不冷凝);最大温度变化:<1℃/分,<10℃/30 分;存储温度:-40℃—60℃;标准内部数据存储:>6 GB 可选外部数据存储: 使用 PC 端口的任何标准 PC 外围设备、USB 端口或以太网端口 雷达系统参数 信噪比:>110 dB 动态范围:>110 dB
数据采集率高达800线秒带天线时45mph70kmh的速度下采集密度为每英寸3d速成数据示例显示管道在1m深处完整的操作系统
Sir20 探地雷达
雷尼绍 RGH24 RGS20 安装指南说明书
Installation guideM-9541-9109-01-EContentsProduct compliance 1 Storage and handling 2 RGH24 readhead installation drawing 3 RGS20 scale installation drawing 4 Scale application 5 End clamps 5 Reference mark and limit switch actuator installation 5 Readhead mounting and alignment 6 Reference mark setup 6 Limit switch 6 Output signals 7 Speed 7 Electrical connections 8 Output specifications 9 General specifications 10 Scale specifications 10Product complianceCRenishaw plc declares that RGH24 complies with the applicable standards and regulations.A copy of the EC Declaration of Conformity is available on request.FCC complianceThis device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) This device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation.The user is cautioned that any changes or modifications not expressly approved by Renishaw plc or authorised representative could void the user’s authority to operate the equipment.This equipment has been tested and found to comply with the limits for a Class A digital device, pursuant to part 15 of the FCC Rules. These limits are designed to provide reasonable protection against harmful interference when the equipment is operated in a commercial environment.This equipment generates, uses, and can radiate radio frequency energy and, if not installedand used in accordance with the instruction manual, may cause harmful interference to radio communications. Operation of this equipment in a residential area is likely to cause harmful interference in which case the user will be required to correct the interference at his own expense.NOTE: This unit was tested with shielded cables on the peripheral devices. Shielded cables must be used with the unit to ensure compliance.Further informationFurther information relating to the RGH24 encoder range can be found in the RGH24 systemData sheet (L-9517-9677). This can be downloaded from our website /encoder and is also available from your local representative. This document may not be copied or reproduced in whole or in part, or transferred to any other media or language, by any means without the written prior permission of Renishaw. The publication of material within this document does not imply freedom from the patent rights of Renishaw plc.DisclaimerRENISHAW HAS MADE CONSIDERABLE EFFORTS TO ENSURE THE CONTENT OF THIS DOCUMENT IS CORRECT AT THE DATE OF PUBLICA TION BUT MAKES NO WARRANTIESOR REPRESENTATIONS REGARDING THE CONTENT. RENISHAW EXCLUDES LIABILITY, HOWSOEVER ARISING, FOR ANY INACCURACIES IN THIS DOCUMENT.The use of this symbol on Renishaw products and/or accompanying documentation indicates that the product should not be mixed with general household waste upon disposal. It is the responsibility of the end user to dispose of this product at a designated collection point for waste electrical and electronic equipment (WEEE) to enable reuse or recycling. Correct disposal of this product will help to save valuable resources and prevent potential negative effects on the environment. For more information, please contact your local waste disposal service or Renishaw distributor.The packaging of our products contains the following materials and can be recycled.REACH regulationInformation required by Article 33(1) of Regulation (EC) No. 1907/2006 (“REACH”) relating to products containing substances of very high concern (SVHCs) is available at:/REACHStorage and handlingRGS20 – 100 mmNOTE: Ensure self-adhesive tape is on outside of bend.Minimum bend radiusOperatingStorageSystem +55 °C 0 °CHumidity95% relative humidity (non-condensing) to EN 60068-2-78N-heptane Propan-2-ol CH 3CHOHCH Acetone3COCH 3Methylated SpiritsChlorinated SolventsRGH24 readhead installation drawing Dimensions and tolerances in mm*Dimensions measured from substrate.†Required nominal 0.8 gap can be set using blue readhead spacer (supplied) positioned between readhead and actuator when positioning/fixing the actuator.‡The recommended thread engagement is 5 mm. The recommended tightening torque is between 0.5 and 0.7 Nm.RGS20 scale installation drawing(with reference mark actuator)Dimensions and tolerances in mmNOTE: The surface roughness of the scale mounting surface must be ≤3.2 Ra. The parallelism of the scale surface to the axis of motion (readhead rideheight variation) must be within 0.05 mm.Bolted reference mark actuator shown(Bolted limit switch actuator shown(Optional epoxy mounted reference mark actuator(A-9531-0250)Optional epoxy mounted limit switch actuator(A-9531-0251)RGS20 scale installation drawing (with limit switch actuator)Dimensions and tolerances in mmScale applicationThe scale applicator A-9541-0124 is designed specifically for use with the RGH24 readheadsand RGS20-S scale. Use applicator A-9541-0305 when installing RGS20-P scale.Allow scale to acclimatize to installation environment prior to installation.Thoroughly clean and degrease the substrate using recommended solvents (see 'Storage and handling').Allow substrate to dry before applying scale. Mark out ‘START’ and ‘FINISH’ points for the scale on the axis substrate. Ensure that there is room for theend clamps (see ‘RGS20 scale installation drawing’). Mount the appropriate scale applicator to the readhead mounting bracket using M2.5 screws. Place the shimsupplied with the readhead between the applicator and substrate to set the nominal height. NOTE:Scale applicator can be mounted either way round to enable easiest orientation for scale installation.Move axis close to scale start position, leaving enough room for the scale to be inserted through theapplicator as shown below. Begin to remove the backing paper from the scale and insert scale into the applicator up to the ‘ST ART’ point(as shown). Ensure backing tape is routed under the splitter screw.End clampsA-9523-4015 is an end clamp kit designed to be used with Renishaw RGS scale.IMPORTANT: End clamps should be used to ensure positional stability of the scale and reference mark repeatability.NOTE: End clamps can be mounted before or after readhead installation.Ensure that excess glue is wiped away from scale as it may affect the readhead signal level.The end clamp features two small regionsof contact adhesive. These will temporarily hold the end clamp in position while the glue cures. Remove the backing tapefrom either side.Remove the lacquer coating from the last15 mm of each end of the scale with a knife and clean with one of the recommended solvents (see ‘Storage and handling’).Immediately position end clamp over theend of the scale. Allow 24 hours at 20 °C for full cure.Thoroughly mix up a sachet of glue(A-9531-0342) and apply a small amount to the underside of the end clamp.Remove applicator and, if necessary, adhere remaining scale manually. Apply firm finger pressure via aclean lint-free cloth along the length of the scale after application to ensure complete adhesion.Clean the scale using Renishaw scale wipes (A-9523-4040) or a clean, dry, lint-free cloth. Fit end clamps (see ‘End clamps’ section).Allow 24 hours for complete adhesion of scale before fitting the reference mark or limit magnet.‘ST ART’ pointSlowly and smoothly move the applicator through the entire axis of travel, ensuring the backing paper ispulled manually from the scale and does not catch under the applicator.Reference mark and limit switch actuator installationScrew mounted or adhesive mounted reference mark and limit switch actuators are available.Refer to RGH24 readhead installation drawing and RGS20 scale installation drawing for actuator positioning.Direction of scale application STARTFor reliable operation, the set-up LED should be GREEN when readhead is moved along the full axis travel.The JST version of the RGH24 has an LED repeater signal that can be used in cases where the LED is not visible.*Remote LED will continuously flash Red when signal <20%Readhead mounting and alignmentMounting bracketsThe bracket must have a flat mounting surface, enable conformance to the installation tolerances, allow adjustment to the rideheight of the readhead, and be sufficiently stiff to prevent deflection or vibration of the readheadduring operation. For easier installation, adjust the roll and yaw of the bracket with respect to the axis of readhead travel before the RGH24 is attached. This can be done with a clock gauge and a precision square.Readhead set-upT o set nominal rideheight, position readhead spacer with ‘L’ shaped aperture under the optical centre of thereadhead to allow normal LED function during set-up procedure. Ensure that the scale, readhead optical window and mounting face are clean and free from obstructions.NOTE: Ensure readhead fixing screws are tightened to 0.5 Nm-0.7 Nm.IMPORTANT: The RGH24 range does not incorporate a separate Alarm ‘E’ signal. Low signal is indicated by a 3-state output of the line driver channels.Reference mark set-upT o ensure unidirectional repeatability, the reference mark requires phasing with the scale in the direction of normal datuming operation.A reference pulse is output in both directions, but repeatabilty is guaranteed only in the phased direction.Ensure readhead is set up correctly with a green LED indication over the full length of travel and that the reference mark actuator is fitted correctly.NOTE: It is recommended that a datum procedure is performed as part of any power-up sequence to ensure the correct datum position is recorded.NOTE: Reference mark output is synchronised with the incremental channels, giving unit of resolution pulse width.Phasing procedureLimit switchA limit switch signal is output when the readhead sensor passes over the magnetic actuator.NOTE: RGH24 readheads are available with reference mark or limit switch detection.Select output at order.NOTE: Limit switch output is not available with analogue RGH24, or options 60, 61 and 62 of the digital RGH24.Output signalsRGH24 D, X, Z, W, Y, H, I, O RS422A digitalRGH24B 1Vpp analogue10 pin JST plug(Termination code Z)15 pin D type plug (Termination code D, L)9 pin D type plug (Termination code A)SpeedDigital readheadsNon-clocked output readheadsNOTE: Maximum speeds of clocked output variants assume 3 m maximum cable length and minimum 5 V supply at readhead connector.Analogue readheadsRGH24B – 4 m/s (−3dB)Clocked output readheadsThe RGH24W, Y , H, I and O readheads are available with a variety of different clocked outputs.Customers must ensure they comply with the lowest recommended counter input frequency.Remote LED driver outputsJST connector version allows for remote monitoring of readhead status.Electrical connections* IMPORTANT: The outer shield should be connected to the machine earth (Field Ground). The inner shield should be connected to 0 V . Care should be taken to ensure that the inner and outer shields are insulated from each other. If the inner and outer shields are connected together, this will cause a short between 0 V and earth, which could cause electrical noise issues.Recommended signal terminationDigital outputs - RGH24D, X, Z, W, Y, H, I and OAnalogue output - RGH24BV 0 V 1 V 2+V 0 V 1 V 2−ΩStandard RS422A line receiver circuitryCapacitors recommended for improved noise immunity.150 Ω+–Output specificationsGeneral specificationsPower supply 5 V ±5%120 mANOTE: Current consumption figures refer to unterminated readheads.For digital outputs a further 25 mA per channel pair (e.g. A+, A−) will bedrawn when terminated with 120 Ω.For analogue outputs a further 20 mA will be drawn when terminatedwith 120 ΩPower from a 5 V dc supply complying with the requirements for SELVof standard IEC BS EN 60950-1.Ripple200 mVpp @frequency up to 500 kHz maximum.Temperature Storage−20 °C to +70 °COperating0 °C to +55 °CHumidity95% relative humidity (non condensing) to EN 60068-2-78Sealing IP40Acceleration Operating500 m/s2, 3 axesShock Non-operating1000 m/s2, 6 ms, ½ sine, 3 axesVibration Operating100 m/s2 max @ 55 Hz to 2000 Hz, 3 axesMass Readhead11 gCable34 g/mCable8 core, double shield, maximum diameter 4.4 mmFlex life >20 × 106 cycles at 20 mm bend radiusThe RGH24 series readheads have been designed to the relevant EMC standards, but must be correctly integrated to achieve EMC compliance. In particular, attention to shielding arrangements is critical. Renishaw recommends the use of a double screened cable to connect RGH24 JST as used in the cable variants of the RGH24Scale specificationsScale type RGS20-S Reflective gold plated steel tape with protective lacquer coating.Adhesive backing tape allows direct mounting to the machine substrate.RGS20-P Reflective gold plated steel tape with tough polyester coating forapplications using harsh solvents.Adhesive backing tape allows direct mounting to the machine substrate. Scale period20 µmLinearity RGS20-S±3 µm/mRGS20-P±5 µm/mScale length Up to 50 m (>50 m by special order)Form(H × W)RGS20-S0.2 mm × 6 mm (includes adhesive)RGS20-P0.3 mm × 6.3 mm (includes adhesive)Substrate materials Metals, ceramics and composites with expansion coefficientsbetween 0 and 22 µm/m/°C(steel, aluminium, Invar, granite, ceramic etc.)Expansion coefficient Matches that of substrate material when scale ends are fixed byepoxy mounted end clampsEnd fixing Epoxy mounted end clamps (A-9523-4015) using 2 part epoxyadhesive (A-9531-0342)Scale end movement typically <1 µm up to +40 °CTemperature Operating−10 °C to +120 °C.Minimum installation10 °CStorage−20 °C to +70 °C.Humidity95% relative humidity (non-condensing) to EN 60068-2-78Renishaw plcNew Mills, Wotton-under-Edge, Gloucestershire GL12 8JR United KingdomT +44 (0)1453 524524F +44 (0)1453 524901E ***************For worldwide contact details,please visit our main website at/contactPart no.: M-9541-9109-01-EIssued: 03.2019 *M-9541-9109-01*RENISHAW HAS MADE CONSIDERABLE EFFORTS TO ENSURE THE CONTENT OF THIS DOCUMENT IS CORRECT A T THE DATE OF PUBLICATION BUT MAKES NO WARRANTIES OR REPRESENTATIONS REGARDING THE CONTENT. RENISHAW EXCLUDES LIABILITY , HOWSOEVER ARISING, FOR ANY INACCURACIES IN THIS DOCUMENT .© 2001-2019 Renishaw plc. All rights reserved.Renishaw reserves the right to change specifications without notice.RENISHAW and the probe symbol used in the RENISHAW logo are registered trade marks of Renishaw plc in the United Kingdom and other countries. apply innovation and names and designations of other Renishaw products and technologies are trade marks of Renishaw plc or its subsidiaries.All other brand names and product names used in this document are trade names, trade marks or registered trade marks of their respective owners.。
SIR-20雷达操作手册 中文版
SIR-20 操作手册美国劳雷工业有限公司第二章二维测量参数设置 (1)2.1: System Parameter Setup 系统参数设置 (1)Create Folders 创建文件夹 (2)Set Program Defaults 设置缺省值 (2)Set working directories 设置工作目录 (3)2.2: Setting Up your System for 2D Data Collection 二维测量 (4)Projects and Profiles: How the SIR-20 Collects Data 项目 (4)The File Header 文件头 (4)Collection Parameters 采集参数设置 (5)2.3: Data Collection Methods 数据采集方法 (7)Survey Wheel Controlled Collection 测量轮控制测量 (7)Position/Range信号位置/时间窗口 (14)Gain增益 (15)Filters and Stacking滤波和叠加 (17)During Collection 数据采集 (18)Time-Based (Free run continuous) Data Collection 连续测量数据采集 (18)Point Mode Data Collection 点测 (19)第二章二维测量参数设置SIR-20地质雷达系统启动后,计算机桌面上有几个radar程序的快捷方式。
基本程序包括数据采集程序SIR-20,现场处理程序RADAN。
图5 SIR-20 桌面SIR-20地质雷达系统有五个快捷方式:RADAN,SIR-20,SS Linescan, Structure Scan, and Optical Scan。
RADAN是后处理程序,其它四个为相互独立的数据采集程序,SIR-20为通用数据采集程序,后三个程序专门采用高频天线检测混凝土结构(详细信息参考第四章)。
Sirios LED 急救灯安装与操作手册说明书
Installation and Operation Manual Sirios LED Emergency Lighting (CG-S)Sirios LED Emergency Lighting - Installation & Operating instructionsStep by step Mounting InstructionsSafety InformationObserve the national safety rules and regulations to prevent accidents as well as the safety instructions included in these instruction lea et.2179SummaryLedpositionApplication Exit Sign Antipanic Escape Route Open (Λ)Closed (ΙΙ)Best*GoodBest**GoodGood Best**** Better uniformity on sign ** Bigger covering area,*** Longer distance in smaller heights, lower illuminance diversity along the route path Open position (Λ)Route, up 4m heightClosed position (II)for Anti-panicSirios LED Emergency Lighting 1-05-255E - Installation & Operation manual 63Conformity with standardsConforms to: EN 60 598-1, EN 60 598-2-22 and DIN EN 1838. Developed, manufactured and tested in accordance with DIN EN ISO 9001.Brief description / Scope of applicationThe emergency light Sirios LED CG-S is suitable for operation on CEAG emergency lighting systems acc. to EN 50 172, DIN VDE 0100-718 and E DIN VDE 0108-100 . The advanced switching and monitoring mode is only available in combination with CEAG CG-S technology.Addressing / Single luminaire monitoringLED converter contolled by a V-CG-S2 monitoring module having 20 addresses for individualmonitoring of luminaire correct operation. Before tting the luminaire, the individual addressing will have to be performed. To do so, the desired address (1-20) is set on the address switch by means of a suitable screw driver. If the luminaire should not be monitored, the code 0/0 has to be selected.Address switch 1 (Tens)000 (1)...2Address switch 2 (Units)012...1...Luminaireaddress Monitoring off 12...11...20Disposal / RecyclingWhen disposing of faulty equipment, observe the valid regulations for recycling and disposal. Plastic parts are marked with the appropriate symbols.Inspection/Maintenance/RepairObserve the valid regulations for theinspection, maintenance and repair of electrical equipment!The light source contained in this luminary shall only be replaced by the manufacturer or his service agent or a similar quali ed person, replacement order code is O-SLED-STRIPE.Sirios LED Emergency Lighting 1-05-255E - Installation & Operation manual Installation / OperationFor the mounting and operation of electrical apparatus, the respective national safetyregulations as well as the general rules ofengineering will have to be observed!Safety NotesŸThe luminaire shall only be used for itsintended purpose and in an indamaged and perfect condition!ŸOnly genuine Eaton spare parts may be used for replacement and repair!ŸWhen working on the emergency luminaire rst the system must be blocked, batteryoperation must be interrupted and mains must ŸPrior to its initial operation, the luminaire will have to be checked in accordance with the instructions as per section ‘Installation’!ŸCarry out the marking of the emergency luminaire:ŸAssign the circuit, the luminaire no. and ID no. and enter them.ŸThe manual log book shall be performed in compliance with the national regulations. It is not applicable by automatical log book!ŸAny foreign matter shall be removed from the luminaire prior to its initial operation!ŸObserve the national safety rules andregulations for prevention of accidents as well operating instructions marked withT echnical DataInput voltage:Power: O-SLED-CG-S Enclosure material:Colour of enclosure: Luminous uxphiE/phiNenn at the end of rated operating time: Supply terminals: Insulation class:Degree of protection acc. to EN 60529: Admissible amb. temperature Lamp:Weight:220-240 V AC, 50/60 Hz, 176 V - 275 V DC33mA AC / 18mA DC PC white100%plug-in terminal 2.5 mm²II IP4200+0C to +40C24 white LED 1.5W 0,77 KgEaton is a registered trademark.All other trademarks are property of their respective owners.© 2015 EatonAll Rights Reserved Printed in EUPublication No. 1-05-255E October 2015Eaton Industries Manufacturing Electrical Sector EMEA Route de la Longeraie 71110 Morges, Switzerland Eaton.euCooper Univel S.A.Thessalonikis 8860134 Katerini, Greece DimensionsSirios171mm357mm153mmSirios weatherproof base。
TL-AC300 V1.0用户手册2.0.0
为普联技术有限公司注册商标。本手册提及的所有商标,由各自所有人拥有。 本手册所提到的产品规格和资讯仅供参考,如有内容更新,恕不另行通知。除非有特殊约定,本手册仅作为 使用指导,所作陈述均不构成任何形式的担保。 Nhomakorabea目录
艾默生SR-20说明书
目录SR-20组成部分 (2)SR-20简要介绍 (3)开始操作介绍 (3)显示内容介绍 (4)设置 (8)SR-20管线探测 (10)探头定位 (15)菜单及其设置 (19)SR-20 组成部分图 1: SR-20 组成部分串行端口USB 接口 序列号标签 图例说明电池仓注:USB/串行端口仅用于上载新软件。
显示屏 按键区 手柄 扬声器折叠夹天线立柱上部天线 折叠铰点导向天线 下部天线SR-20 简要介绍开始操作介绍安装/更换电池把SR-20倒过来会找到用于提供电力的电池仓。
首先逆时针转动旋钮打开仓盖,按照正负极标记装入电池,盖上仓盖,轻压顺时针转动旋钮。
图2: 电池仓当启动SR-20时,它会花几秒钟来检测电池电量。
如果电池用完,它会显示为“empty”(空)。
折叠天线杆开始操作前,展开折叠天线至铰点处锁住。
当完成定位工作时,按下红色释放按钮,折叠天线以便于存放。
注:当进行定位操作时,避免使下部天线在地面拖行。
因为这样会导致噪音信号,影响定位结果,并最终可能导致天线损坏。
释放按钮图3: 折叠天线杆和释放按钮SR-20 探测模式SR-20 有三种截然不同的探测模式. 它们是:1. 有源探测模式,通过信号发生机,选定一个频率施加于一段较长的导体上,用于探测具有导电性能的管道、管线或电缆。
2. 无源探测模式,用于探测50Hz或60Hz的电力电线,或无线电频率探测。
3. 发射探头探测模式,用于探测非金属管道、沟渠或隧道内的发射探头或者不能被前两种模式探测到的地方。
注:两种管线探测模式─有源和无源,除了所用的频率不同外,其他原理都是一样的。
在无源模式下不会用到信号发射机。
显示内容介绍对于初次使用定位仪的用户或经验丰富的用户,都同样可以轻易上手使用SR-20。
SR-20提供许多先进的特性和参数,使得大多数复杂的定位工作变得非常容易。
此外,当你在不复杂的环境下完成一些最基本的定位工作时,这些特性和参数还可以关闭或隐藏,从而使得显示内容一目了然。
HC32L130_HC32L136系列用户手册Rev1.4
HC32L130系列/ HC32L136系列32位ARM® Cortex®-M0+ 微控制器用户手册前言非常感谢大家对华大半导体产品的支持和信赖。
使用本系列产品前,请系统阅读本手册和“数据手册”。
➢本手册的目的和对象读者本手册主要介绍本系列的功能、操作事项和使用方法。
对象读者为使用本系列实际开发产品的工程师。
※本手册介绍外设功能的构成和操作说明,但不包括该系列的规格说明。
关于芯片规格,详情参见其对应的“数据手册”。
➢样本程序和开发环境华大半导体提供外设功能运行用的样本程序和本系列所需的开发环境说明。
关于华大微控制器的运行规格和使用方法,请联系本公司。
➢微控制器支持信息:/mcu.htm©2019 华大半导体有限公司- 保留所有权利目录前言 (2)目录 (3)简介 (34)产品特性超低功耗MCU (35)1功能模块 (36)1.132 位CORTEX M0+ 内核 (37)1.264K Byte FLASH (37)1.38K Byte RAM (37)1.4时钟系统 (37)1.5工作模式 (38)1.6硬件实时时钟RTC (38)1.7通用IO 端口 (38)1.8中断控制器 (38)1.9复位控制器 (39)1.10DMAC (40)1.11定时器/计数器 (40)1.12超低功耗脉冲计数器PCNT (42)1.13看门狗WDT (43)1.14通用异步收发器UART0~UART1 (43)1.15低功耗异步收发器LPUART0~LPUART1 (43)1.16同步串行接口SPI (44)1.17I2C 总线 (44)1.18蜂鸣器Buzzer (45)1.19时钟校准电路 (45)1.20唯一识别号UID (45)1.21CRC16/32 硬件循环冗余校验码 (45)1.2232位硬件除法器 (46)1.23AES 硬件加密 (46)1.24TRNG 真随机数发生器 (46)1.2512 Bit SARADC (46)1.26电压比较器VC (47)1.27低电压检测器LVD (47)1.28运放OPA (48)1.29LCD 驱动 (48)1.30嵌入式调试系统 (48)1.31在线编程模式 (49)1.32高安全性 (49)2引脚配置及功能 (50)2.1封装示意图 (50)2.2引脚功能说明 (54)3系统结构 (64)3.1概述 (64)3.2系统地址划分 (65)3.3存储器和模块地址分配 (66)4工作模式 (68)4.1运行模式 (70)4.2休眠模式 (72)4.3深度休眠模式 (74)5系统控制器(SYSCTRL) (77)5.1系统时钟介绍 (77)5.1.1内部高速RC时钟RCH (78)5.1.2内部低速RC 时钟RCL (78)5.1.3外部低速晶振时钟XTL (79)5.1.4外部高速晶振时钟XTH (79)5.1.5锁相环时钟PLL (79)5.1.6时钟启动过程 (80)5.2系统时钟切换 (81)5.2.1标准的时钟切换流程 (81)5.2.2RCH不同振荡频率间切换流程 (82)5.2.3从其它时钟切换到XTL示例 (82)5.2.4从其它时钟切换到XTH示例 (83)5.2.5从其它时钟切换到RCL示例 (83)5.2.6从其它时钟切换到RCH示例 (84)5.2.7PLL与RCH相互切换示例,参考时钟为RCH (84)5.2.8PLL与XTH相互切换示例,参考时钟为XTH (85)5.3时钟校准模块 (86)5.4中断唤醒控制 (88)5.4.1从深度休眠模式唤醒后执行中断服务程序的方法 (88)5.4.2从深度休眠模式唤醒后不执行中断服务程序的方法 (88)5.4.3使用退出休眠特性 (89)5.5寄存器 (91)5.5.1系统控制寄存器0(SYSCTRL0) (92)5.5.2系统控制寄存器1(SYSCTRL1) (94)5.5.3系统控制寄存器2(SYSCTRL2) (96)5.5.4RCH 控制寄存器(RCH_CR) (97)5.5.5XTH 控制寄存器(XTH_CR) (98)5.5.6RCL 控制寄存器(RCL_CR) (99)5.5.7XTL 控制寄存器(XTL_CR) (100)5.5.8PLL 控制寄存器(PLL_CR) (101)5.5.9外围模块时钟控制寄存器(PERI_CLKEN) (103)6复位控制器(RESET) (105)6.1.1上电下电复位POR (105)6.1.2外部复位引脚复位 (106)6.1.3WDT复位 (106)6.1.4PCA复位 (106)6.1.5LVD低电压复位 (106)6.1.6Cortex-M0+ SYSRESETREQ复位 (106)6.1.7Cortex-M0+ LOCKUP复位 (106)6.2寄存器 (107)6.2.1复位标识寄存器(RESET_FLAG) (107)6.2.2外围模块复位控制寄存器(PREI_RESET) (109)7中断控制器(NVIC) (111)7.1概述 (111)7.2中断优先级 (111)7.3中断向量表 (112)7.4中断输入和挂起行为 (113)7.5中断等待 (116)7.6中断源 (117)7.7中断结构图 (119)7.8寄存器 (121)7.8.1中断使能设置寄存器(SCS_SETENA) (121)7.8.2中断使能清除寄存器(SCS_CLRENA) (122)7.8.3中断挂起状态设置寄存器(SCS_SETPEND) (122)7.8.4中断挂起状态清除寄存器(SCS_CLRPEND) (123)7.8.5中断优先级寄存器(SCS_IPR0) (124)7.8.6中断优先级寄存器(SCS_IPR1) (125)7.8.7中断优先级寄存器(SCS_IPR2) (126)7.8.8中断优先级寄存器(SCS_IPR3) (127)7.8.9中断优先级寄存器(SCS_IPR4) (128)7.8.10中断优先级寄存器(SCS_IPR5) (129)7.8.11中断优先级寄存器(SCS_IPR6) (130)7.8.12中断优先级寄存器(SCS_IPR7) (131)7.8.13中断屏蔽特殊寄存器(SCS_PRIMASK) (132)7.9软件基本操作 (133)7.9.1外部中断使能 (133)7.9.2NVIC 中断使能和清除使能 (133)7.9.3NVIC 中断挂起和清除挂起 (133)7.9.4NVIC 中断优先级 (133)7.9.5NVIC 中断屏蔽 (134)8端口控制器(GPIO) (135)8.1端口控制器简介 (135)8.2端口控制器主要特性 (135)8.3.1端口配置功能 (136)8.3.2端口数字复用功能 (138)8.3.3端口中断功能 (140)8.4端口配置操作流程 (141)8.4.1端口复用配置为模拟端口操作流程 (141)8.4.2端口复用配置为数字通用端口操作流程 (141)8.4.3端口复用配置为数字功能端口操作流程 (141)8.4.4端口复用配置为调试测试端口操作流程 (141)8.4.5端口复用配置为红外输出信号操作流程 (141)8.4.6端口高电平中断操作流程 (142)8.4.7端口低电平中断操作流程 (142)8.4.8端口上升沿中断操作流程 (142)8.4.9端口下降沿中断操作流程 (142)8.4.10端口上拉使能配置操作流程 (143)8.4.11端口下拉使能配置操作流程 (143)8.4.12端口增强驱动配置操作流程 (143)8.4.13端口开漏输出配置操作流程 (143)8.4.14端口位置位操作流程 (143)8.4.15端口位清零操作流程 (143)8.4.16端口位置位清零操作流程 (143)8.5端口控制器寄存器描述 (144)8.5.1端口PA (148)8.5.1.1端口PA00功能配置寄存器(PA00_SEL) (148)8.5.1.2端口PA01功能配置寄存器(PA01_SEL) (149)8.5.1.3端口PA02功能配置寄存器(PA02_SEL) (150)8.5.1.4端口PA03功能配置寄存器(PA03_SEL) (151)8.5.1.5端口PA04功能配置寄存器(PA04_SEL) (152)8.5.1.6端口PA05功能配置寄存器(PA05_SEL) (153)8.5.1.7端口PA06功能配置寄存器(PA06_SEL) (154)8.5.1.8端口PA07功能配置寄存器(PA07_SEL) (155)8.5.1.9端口PA08功能配置寄存器(PA08_SEL) (156)8.5.1.10端口PA09功能配置寄存器(PA09_SEL) (157)8.5.1.11端口PA10功能配置寄存器(PA10_SEL) (158)8.5.1.12端口PA11功能配置寄存器(PA11_SEL) (159)8.5.1.13端口PA12功能配置寄存器(PA12_SEL) (160)8.5.1.14端口PA13功能配置寄存器(PA13_SEL) (161)8.5.1.15端口PA14功能配置寄存器(PA14_SEL) (162)8.5.1.16端口PA15功能配置寄存器(PA15_SEL) (163)8.5.1.17端口PA输入输出配置寄存器(PADIR) (164)8.5.1.18端口PA输入值寄存器(PAIN) (165)8.5.1.19端口PA输出值配置寄存器(PAOUT) (166)8.5.1.20端口PA数模配置寄存器(PAADS) (167)8.5.1.21端口PA位置位寄存器(PABSET) (168)8.5.1.22端口PA位清零寄存器(PABCLR) (169)8.5.1.23端口PA位置位清零寄存器(PABSETCLR) (170)8.5.1.24端口PA驱动能力配置寄存器(PADR) (171)8.5.1.25端口PA上拉使能配置寄存器(PAPU) (172)8.5.1.26端口PA下拉使能配置寄存器(PAPD) (173)8.5.1.27端口PA开漏输出配置寄存器(PAOD) (174)8.5.1.28端口PA高电平中断使能配置寄存器(PAHIE) (175)8.5.1.29端口PA低电平中断使能配置寄存器(PALIE) (176)8.5.1.30端口PA上升沿中断使能配置寄存器(PARIE) (177)8.5.1.31端口PA下降沿中断使能配置寄存器(PAFIE) (178)8.5.1.32端口PA中断状态寄存器(PA_STA T) (179)8.5.1.33端口PA中断清除寄存器(PA_ICLR) (180)8.5.2端口PB (181)8.5.2.1端口PB00功能配置寄存器(PB00_SEL) (181)8.5.2.2端口PB01功能配置寄存器(PB01_SEL) (182)8.5.2.3端口PB02功能配置寄存器(PB02_SEL) (183)8.5.2.4端口PB03功能配置寄存器(PB03_SEL) (184)8.5.2.5端口PB04功能配置寄存器(PB04_SEL) (185)8.5.2.6端口PB05功能配置寄存器(PB05_SEL) (186)8.5.2.7端口PB06功能配置寄存器(PB06_SEL) (187)8.5.2.8端口PB07功能配置寄存器(PB07_SEL) (188)8.5.2.9端口PB08功能配置寄存器(PB08_SEL) (189)8.5.2.10端口PB09功能配置寄存器(PB09_SEL) (190)8.5.2.11端口PB10功能配置寄存器(PB10_SEL) (191)8.5.2.12端口PB11功能配置寄存器(PB11_SEL) (192)8.5.2.13端口PB12功能配置寄存器(PB12_SEL) (193)8.5.2.14端口PB13功能配置寄存器(PB13_SEL) (194)8.5.2.15端口PB14功能配置寄存器(PB14_SEL) (195)8.5.2.16端口PB15功能配置寄存器(PB15_SEL) (196)8.5.2.17端口PB输入输出配置寄存器(PBDIR) (197)8.5.2.18端口PB输入值寄存器(PBIN) (198)8.5.2.19端口PB输出值配置寄存器(PBOUT) (199)8.5.2.20端口PB数模配置寄存器(PBADS) (200)8.5.2.21端口PB位置位寄存器(PBBSET) (201)8.5.2.22端口PB位清零寄存器(PBBCLR) (202)8.5.2.23端口PB位置位清零寄存器(PBBSETCLR) (203)8.5.2.24端口PB驱动能力配置寄存器(PBDR) (204)8.5.2.25端口PB上拉使能配置寄存器(PBPU) (205)8.5.2.26端口PB下拉使能配置寄存器(PBPD) (206)8.5.2.27端口PB开漏输出配置寄存器(PBOD) (207)8.5.2.29端口PB低电平中断使能配置寄存器(PBLIE) (209)8.5.2.30端口PB上升沿中断使能配置寄存器(PBRIE) (210)8.5.2.31端口PB下降沿中断使能配置寄存器(PBFIE) (211)8.5.2.32端口PB中断状态寄存器(PB_STA T) (212)8.5.2.33端口PB中断清除寄存器(PB_ICLR) (213)8.5.3端口PC (214)8.5.3.1端口PC00功能配置寄存器(PC00_SEL) (214)8.5.3.2端口PC01功能配置寄存器(PC01_SEL) (215)8.5.3.3端口PC02功能配置寄存器(PC02_SEL) (216)8.5.3.4端口PC03功能配置寄存器(PC03_SEL) (217)8.5.3.5端口PC04功能配置寄存器(PC04_SEL) (218)8.5.3.6端口PC05功能配置寄存器(PC05_SEL) (219)8.5.3.7端口PC06功能配置寄存器(PC06_SEL) (220)8.5.3.8端口PC07功能配置寄存器(PC07_SEL) (221)8.5.3.9端口PC08功能配置寄存器(PC08_SEL) (222)8.5.3.10端口PC09功能配置寄存器(PC09_SEL) (223)8.5.3.11端口PC10功能配置寄存器(PC10_SEL) (224)8.5.3.12端口PC11功能配置寄存器(PC11_SEL) (225)8.5.3.13端口PC12功能配置寄存器(PC12_SEL) (226)8.5.3.14端口PC13功能配置寄存器(PC13_SEL) (227)8.5.3.15端口PC14功能配置寄存器(PC14_SEL) (228)8.5.3.16端口PC15功能配置寄存器(PC15_SEL) (229)8.5.3.17端口PC输入输出配置寄存器(PCDIR) (230)8.5.3.18端口PC输入值寄存器(PCIN) (231)8.5.3.19端口PC输出值配置寄存器(PCOUT) (232)8.5.3.20端口PC数模配置寄存器(PCADS) (233)8.5.3.21端口PC位置位寄存器(PCBSET) (234)8.5.3.22端口PC位清零寄存器(PCBCLR) (235)8.5.3.23端口PC位置位清零寄存器(PCBSETCLR) (236)8.5.3.24端口PC驱动能力配置寄存器(PCDR) (237)8.5.3.25端口PC上拉使能配置寄存器(PCPU) (238)8.5.3.26端口PC下拉使能配置寄存器(PCPD) (239)8.5.3.27端口PC开漏输出配置寄存器(PCOD) (240)8.5.3.28端口PC高电平中断使能配置寄存器(PCHIE) (241)8.5.3.29端口PC低电平中断使能配置寄存器(PCLIE) (242)8.5.3.30端口PC上升沿中断使能配置寄存器(PCRIE) (243)8.5.3.31端口PC下降沿中断使能配置寄存器(PCFIE) (244)8.5.3.32端口PC中断状态寄存器(PC_STAT) (245)8.5.3.33端口PC中断清除寄存器(PC_ICLR) (246)8.5.4端口PD (247)8.5.4.1端口PD00功能配置寄存器(PD00_SEL) (247)8.5.4.3端口PD02功能配置寄存器(PD02_SEL) (249)8.5.4.4端口PD03功能配置寄存器(PD03_SEL) (250)8.5.4.5端口PD04功能配置寄存器(PD04_SEL) (251)8.5.4.6端口PD05功能配置寄存器(PD05_SEL) (252)8.5.4.7端口PD06功能配置寄存器(PD06_SEL) (253)8.5.4.8端口PD07功能配置寄存器(PD07_SEL) (254)8.5.4.9端口PD输入输出配置寄存器(PDDIR) (255)8.5.4.10端口PD输入值寄存器(PDIN) (256)8.5.4.11端口PD输出值配置寄存器(PDOUT) (257)8.5.4.12端口PD数模配置寄存器(PDADS) (258)8.5.4.13端口PD位置位寄存器(PDBSET) (259)8.5.4.14端口PD位清零寄存器(PDBCLR) (260)8.5.4.15端口PD位置位清零寄存器(PDBSETCLR) (261)8.5.4.16端口PD驱动能力配置寄存器(PDDR) (262)8.5.4.17端口PD上拉使能配置寄存器(PDPU) (263)8.5.4.18端口PD下拉使能配置寄存器(PDPD) (264)8.5.4.19端口PD开漏输出配置寄存器(PDOD) (265)8.5.4.20端口PD高电平中断使能配置寄存器(PDHIE) (266)8.5.4.21端口PD低电平中断使能配置寄存器(PDLIE) (267)8.5.4.22端口PD上升沿中断使能配置寄存器(PDRIE) (268)8.5.4.23端口PD下降沿中断使能配置寄存器(PDFIE) (269)8.5.4.24端口PD中断状态寄存器(PD_STAT) (270)8.5.4.25端口PD中断清除寄存器(PD_ICLR) (271)8.5.5端口辅助功能 (272)8.5.5.1端口辅助功能配置寄存器0(GPIO_CTRL0) (272)8.5.5.2端口辅助功能配置寄存器1(GPIO_CTRL1) (273)8.5.5.3端口辅助功能配置寄存器2(GPIO_CTRL2) (275)8.5.5.4端口辅助功能定时器门控选择(GPIO_TIMGS) (276)8.5.5.5端口辅助功能定时器ETR选择(GPIO_TIMES) (277)8.5.5.6端口辅助功能定时器捕获输入选择(GPIO_TIMCPS) (278)8.5.5.7端口辅助功能PCA捕获选择(GPIO_PCAS) (279)9I2C总线(I2C) (280)9.1I2C 简介 (280)9.2I2C 主要特性 (280)9.3I2C 协议描述 (281)9.3.1I2C 总线上数据传输 (281)9.3.2起始位或重复起始信号 (282)9.3.3从机地址传输 (282)9.3.4数据传输 (282)9.4I2C 功能描述 (284)9.4.1I2C 工作模式 (285)9.4.2仲裁与同步逻辑 (285)9.4.3串行时钟发生器 (286)9.4.4输入滤波器 (286)9.4.5地址比较器 (286)9.4.6中断产生器 (287)9.4.7I2C 主机发送模式 (287)9.4.8I2C 主机接收模式 (290)9.4.9I2C 从机接收模式 (292)9.4.10I2C 从机发送模式 (296)9.4.11I2C 其他杂项状态 (298)9.5I2C 操作模式 (299)9.5.1初始化程序 (299)9.5.2启动主机发送功能 (299)9.5.3启动主机接收功能 (299)9.5.4I2C中断程序 (300)9.5.5无指定模式的状态 (300)9.5.6主发送器状态 (301)9.5.7主接收状态 (302)9.5.8从接收器状态 (303)9.5.9从发送器状态 (305)9.6I2C寄存器描述 (308)9.6.1I2C波特率计数器使能寄存器(I2Cx_TMRUN) (308)9.6.2I2C波特率计数器配置寄存器(I2Cx_TM) (309)9.6.3I2C配置寄存器(I2Cx_CR) (310)9.6.4I2C数据寄存器(I2Cx_DATA) (311)9.6.5I2C地址寄存器(I2Cx_ADDR) (312)9.6.6I2C状态寄存器(I2Cx_STAT) (313)10串行外设接口(SPI) (314)10.1SPI 简介 (314)10.2SPI 主要特性 (314)10.3SPI 功能描述 (315)10.3.1SPI 主机查询方式 (315)10.3.2SPI 主机DMA方式 (316)10.3.3SPI 主机数据时钟时序 (317)10.3.4SPI 从机查询方式 (318)10.3.5SPI 从机DMA方式 (319)10.3.6SPI 从机数据时钟时序 (320)10.4SPI 中断 (321)10.5SPI 多主机/多从机系统的配置 (322)10.6SPI 引脚配置说明 (323)10.7SPI 寄存器描述 (324)10.7.1SPI配置寄存器(SPIx_CR) (325)10.7.2SPI片选配置寄存器(SPIx_SSN) (326)10.7.3SPI状态寄存器(SPIx_STA T) (327)10.7.4SPI数据寄存器(SPIx_DA TA) (328)10.7.5SPI配置寄存器2(SPIx_CR2) (329)10.7.6SPI中断清除寄存器2(SPIx_ICLR) (330)11时钟校准模块(CLKTRIM) (331)11.1CLKTRIM 简介 (331)11.2CLKTRIM主要特性 (331)11.3CLKTRIM功能描述 (332)11.3.1CLKTRIM校准模式 (332)11.3.1.1时钟校准原理 (332)11.3.1.2时钟校准模块硬件结构 (332)11.3.1.3时钟校准软件流程 (333)11.3.2CLKTRIM监测模式 (335)11.3.2.1时钟监测原理 (335)11.3.2.2时钟监测硬件结构 (335)11.3.2.3时钟监测软件流程 (335)11.4CLKTRIM寄存器描述 (338)11.4.1配置寄存器(CLKTRIM_CR) (339)11.4.2参考计数器初值配置寄存器(CLKTRIM_REFCON) (341)11.4.3参考计数器值寄存器(CLKTRIM_REFCNT) (341)11.4.4校准计数器值寄存器(CLKTRIM_CALCNT) (342)11.4.5中断标志位寄存器(CLKTRIM_IFR) (343)11.4.6中断标志位清除寄存器(CLKTRIM_ICLR) (344)11.4.7校准计数器溢出值配置寄存器(CLKTRIM_CALCON) (345)12硬件除法器模块(HDIV) (346)12.1HDIV 简介 (346)12.2HDIV主要特性 (346)12.3HDIV功能描述 (347)12.3.1HDIV操作流程 (347)12.4HDIV寄存器描述 (348)12.4.1被除数寄存器(HDIV_DIVIDEND) (348)12.4.2除数寄存器(HDIV_DIVISOR) (349)12.4.3商寄存器(HDIV_QUOTIENT) (349)12.4.4余数寄存器(HDIV_REMAINDER) (350)12.4.5符号寄存器(HDIV_SIGN) (350)12.4.6状态寄存器(HDIV_STAT) (351)13FLASH控制器(FLASH) (352)13.1概述 (352)13.2FLASH容量划分 (352)13.3功能描述 (353)13.3.1页擦除(Sector Erase) (353)13.3.3写操作(Program) (355)13.3.4读操作(Read) (357)13.4擦写时间 (358)13.5读等待周期 (360)13.6擦写保护 (360)13.6.1擦写保护位 (360)13.6.2PC地址擦写保护 (360)13.7寄存器写保护 (361)13.8寄存器 (362)13.8.1TNVS参数寄存器(FLASH_TNVS) (362)13.8.2TPGS参数寄存器(FLASH_TPGS) (363)13.8.3TPROG参数寄存器(FLASH_TPROG) (363)13.8.4TSERASE寄存器(FLASH_TSERASE) (364)13.8.5TMERASE参数寄存器(FLASH_TMERASE) (364)13.8.6TPRCV参数寄存器(FLASH_TPRCV) (365)13.8.7TSRCV参数寄存器(FLASH_TSRCV) (365)13.8.8TMRCV参数寄存器(FLASH_TMRCV) (366)13.8.9CR寄存器(FLASH_CR) (367)13.8.10IFR寄存器(FLASH_IFR) (368)13.8.11ICLR寄存器(FLASH_ICLR) (368)13.8.12BYPASS寄存器(FLASH_BYPASS) (369)13.8.13SLOCK寄存器(FLASH_SLOCK) (369)14RAM控制器(RAM) (370)14.1概述 (370)14.2功能描述 (370)14.2.1RAM地址范围 (370)14.2.2读写位宽 (371)14.2.3奇偶校验 (371)14.3寄存器 (372)14.3.1控制寄存器(RAM_CR) (372)14.3.2奇偶校验出错地址寄存器(RAM_ERRADDR) (373)14.3.3出错中断标志寄存器(RAM_IFR) (373)14.3.4出错中断标志清除寄存器(RAM_ICLR) (374)15DMA控制器(DMAC) (375)15.1概述 (375)15.2功能框图 (377)15.3基本功能 (380)15.3.1软件-块(Block)传输 (380)15.3.2软件-突发(Burst)传输 (383)15.3.3硬件-块(Block)传输 (385)15.3.4硬件-突发(Burst)传输 (386)15.4寄存器 (388)15.4.1DMAC_CONF (389)15.4.2DMAC_CONFA0、DMAC_CONFA1 (390)15.4.3DMAC_CONFB0、DMAC_CONFB1 (392)15.4.4DMAC_SRCADR0、DMAC_SRCADR1 (394)15.4.5DMAC_DSTADR0、DMAC_DSTADR1 (395)16通用定时器(TIM0/1/2/3) (396)16.1通用定时器简介 (396)16.1.1基本特性(TIM0/1/2) (396)16.1.2基本特性(TIM3) (398)16.2Timer 功能描述 (399)16.2.1定时计数器 (399)16.2.2定时器预除频 (399)16.2.3模式0 计数定时器功能 (399)16.2.3.1功能框图 (400)16.2.3.2计数波形 (401)16.2.3.3计数功能 (402)16.2.3.4定时功能 (402)16.2.3.5时序图 (402)16.2.3.6Buzzer功能 (403)16.2.3.7设置示例 (404)16.2.4模式1 脉宽测量PWC (405)16.2.4.1PWC功能框图 (405)16.2.4.2PWC波形测量时序图 (406)16.2.4.3PWC单次触发模式 (408)16.2.4.1设置示例 (408)16.2.5模式2/3比较捕获模式 (410)16.2.5.1计数器 (410)16.2.5.2计数器波形 (411)16.2.5.3重复计数 (414)16.2.5.4数据缓存 (415)16.2.5.5比较输出OCREF (419)16.2.5.6独立PWM输出 (422)16.2.5.7互补PWM输出 (423)16.2.5.8有死区的PWM输出 (424)16.2.5.9单脉冲输出 (425)16.2.5.10比较中断 (426)16.2.5.11捕获输入 (427)16.2.5.12设置示例 (430)16.2.6模式2/3从模式 (433)16.2.6.1门控计数 (433)16.2.6.2触发功能 (434)16.2.6.3复位计数 (434)16.2.7正交编码计数功能 (435)16.2.8Timer触发ADC (437)16.2.9刹车控制 (438)16.2.10Timer 互联 (438)16.2.11GATE输入互联 (439)16.2.12ETR输入互联 (439)16.2.13CHx捕获输入互联 (440)16.2.14DMA (440)16.2.14.1设置示例 (442)16.3Timer 寄存器描述 (443)16.4模式0定时器寄存器描述 (444)16.4.116位模式重载寄存器(TIMx_ARR) (444)16.4.216位模式计数寄存器(TIMx_CNT) (444)16.4.332位模式计数寄存器(TIMx_CNT32) (445)16.4.4控制寄存器(TIMx_M0CR) (446)16.4.5中断标志寄存器(TIMx_IFR) (448)16.4.6中断标志清除寄存器(TIMx_ICLR) (448)16.4.7死区时间寄存器(TIMx_DTR) (449)16.5脉冲宽度测量PWC寄存器描述 (450)16.5.116位模式计数寄存器(TIMx_CNT) (450)16.5.2控制寄存器(TIMx_M1CR) (451)16.5.3中断标志寄存器(TIMx_IFR) (453)16.5.4中断标志清除寄存器(TIMx_ICLR) (453)16.5.5主从模式控制寄存器(TIMx_MSCR) (454)16.5.6输出控制滤波(TIMx_FLTR) (455)16.5.7控制寄存器(TIMx_CR0) (456)16.5.8比较捕获寄存(TIMx_CCR0A ) (456)16.6模式2,3寄存器描述 (457)16.6.116位模式重载寄存器(TIMx_ARR) (457)16.6.216位模式计数寄存器(TIMx_CNT) (457)16.6.3控制寄存器(TIMx_M23CR) (458)16.6.4中断标志寄存器(TIMx_IFR) (461)16.6.5中断标志清除寄存器(TIMx_ICLR) (463)16.6.6主从模式控制寄存器(TIMx_MSCR) (464)16.6.7输出控制/输入滤波(TIMx_FLTR) (466)16.6.8ADC触发控制寄存器(TIMx_ADTR) (469)16.6.9通道0控制寄存器(TIMx_CRCH0) (470)16.6.10通道1/2控制寄存器(TIM3_CRCH1/2)(仅TIM3存在) (472)16.6.11死区时间寄存器(TIMx_DTR) (474)16.6.12重复周期设置值(TIMx_RCR) (476)16.6.13通道0比较捕获寄存器(TIMx_CCR0A/B) (477)16.6.14通道1/2比较捕获寄存器(TIM3_CCR1/2 A/B) (仅TIM3存在) (478)17低功耗定时器(LPTIM) (479)17.1LPTimer 简介 (479)17.2LPTimer 功能描述 (480)17.2.1计数功能 (481)17.2.2定时功能 (481)17.3LPTimer 互连 (482)17.3.1GATE互联 (482)17.3.2EXT互联 (482)17.3.3Toggle输出互联 (483)17.4LPTimer 寄存器描述 (484)17.4.1计数器计数值寄存器(LPTIM_CNT) (485)17.4.2重载寄存器(LPTIM_ARR) (485)17.4.3控制寄存器(LPTIM_CR) (486)17.4.4中断标志寄存器(LPTIM_IFR) (487)17.4.5中断标志清除寄存器(LPTIM_ICLR) (487)18可编程计数阵列(PCA) (488)18.1PCA简介 (488)18.2PCA功能描述 (489)18.2.1PCA定时/计数器 (490)18.2.1.116位自由计数模式 (491)18.2.1.216位重载计数模式 (491)18.2.2PCA捕获功能 (493)18.2.3PCA比较功能 (495)18.2.3.1比较翻转输出模式 (495)18.2.3.2PCA 16位PWM功能 (497)18.2.3.3PCA模块4的WDT功能 (498)18.2.3.4PCA 8位PWM功能 (499)18.3PCA模块与其他模块互连及控制 (502)18.4PCA寄存器描述 (503)18.4.1控制寄存器(PCA_CCON) (504)18.4.2模式寄存器(PCA_CMOD) (505)18.4.3计数寄存器(PCA_CNT) (506)18.4.4中断清除寄存器(PCA_ICLR) (506)18.4.5比较捕获模式寄存器(PCA_CCAPM0~4) (507)18.4.6比较捕获数据寄存器高8位(PCA_CCAP0~4H) (508)18.4.7比较捕获数据寄存器低8位(PCA_CCAP0~4L) (508)18.4.8比较捕获16位寄存器(PCA_CCAP0~4) (509)18.4.9比较高速输出标志寄存器(PCA_CCAPO) (509)18.4.10周期寄存器(PCA_CARR) (510)18.4.11增强PWM控制(PCA_EPWM) (510)19高级定时器(TIM4/5/6) (511)19.1Advanced Timer 简介 (511)19.2Advanced Timer 功能描述 (513)19.2.1基本动作 (513)19.2.1.1基本波形模式 (513)19.2.1.2比较输出 (514)19.2.1.3捕获输入 (515)19.2.2时钟源选择 (515)19.2.3计数方向 (516)19.2.3.1锯齿波计数方向 (516)19.2.3.2三角波计数方向 (516)19.2.4数字滤波 (516)19.2.5软件同步 (517)19.2.5.1软件同步启动 (517)19.2.5.2软件同步停止 (518)19.2.5.3软件同步清零 (518)19.2.6硬件同步 (518)19.2.6.1硬件同步启动 (518)19.2.6.2硬件同步停止 (518)19.2.6.3硬件同步清零 (519)19.2.6.4硬件同步捕获输入 (519)19.2.6.5硬件同步计数 (520)19.2.7缓存功能 (521)19.2.7.1缓存传送时间点 (522)19.2.7.2通用周期基准值缓存传送时间点 (522)19.2.7.3通用比较基准值缓存传送时间点 (522)19.2.7.4捕获输入值缓存传送时间点 (522)19.2.7.5清零动作时缓存传送 (522)19.2.8通用PWM输出 (523)19.2.8.1PWM展频输出 (523)19.2.8.2独立PWM输出 (523)19.2.8.3互补PWM输出 (524)19.2.8.4多相PWM输出 (526)19.2.9正交编码计数 (528)19.2.9.1位置计数模式 (528)19.2.9.2公转模式 (531)19.2.10周期间隔响应 (534)19.2.11保护机制 (534)19.2.12中断说明 (535)19.2.12.1计数比较匹配中断 (535)19.2.12.2计数周期匹配中断 (535)19.2.12.3死区时间错误中断 (535)19.2.13DMA (536)19.2.14刹车保护 (536)19.2.14.1端口刹车与软件刹车 (536)19.2.14.2低功耗模式自动刹车 (537)19.2.14.3输出电平同高同低刹车 (537)19.2.14.4VC 刹车 (537)19.2.15内部互连 (539)19.2.15.1中断触发输出 (539)19.2.15.2AOS 触发 (540)19.2.15.3端口触发TRIGA-TRIGD (541)19.2.15.4比较输出VC 与Advanced Timer 互连 (541)19.3寄存器描述 (542)19.3.1通用计数基准值寄存器(TIMx_CNTER) (544)19.3.2通用周期基准值寄存器(TIMx_PERAR) (544)19.3.3通用周期缓存寄存器(TIMx_PERBR) (545)19.3.4通用比较基准值寄存器(TIMx_GCMAR-GCMDR) (545)19.3.5专用比较基准值寄存器(TIMx_SCMAR-SCMBR) (546)19.3.6死区时间基准值寄存器(TIMx_DTUAR- DTDAR) (546)19.3.7通用控制寄存器(TIMx_GCONR) (547)19.3.8中断控制寄存器(TIMx_ICONR) (549)19.3.9端口控制寄存器(TIMx_PCONR) (551)19.3.10缓存控制寄存器(TIMx_BCONR) (554)19.3.11死区控制寄存器(TIMx_DCONR) (555)19.3.12滤波控制寄存器(TIMx_FCONR) (556)19.3.13有效周期寄存器(TIMx_VPERR) (558)19.3.14状态标志寄存器(TIMx_STFLR) (559)19.3.15硬件启动事件选择寄存器(TIMx_HSTAR) (561)19.3.16硬件停止事件选择寄存器(TIMx_HSTPR) (563)19.3.17硬件清零事件选择寄存器(TIMx_HCELR) (565)19.3.18硬件捕获A事件选择寄存器(TIMx_HCPAR) (567)19.3.19硬件捕获B事件选择寄存器(TIMx_HCPBR) (569)19.3.20硬件递加事件选择寄存器(TIMx_HCUPR) (571)19.3.21硬件递减事件选择寄存器(TIMx_HCDOR) (573)19.3.22软件同步启动寄存器(TIMx_SSTAR) (575)19.3.23软件同步停止寄存器(TIMx_SSTPR) (576)19.3.24软件同步清零寄存器(TIMx_SCLRR) (577)19.3.25中断标志寄存器(TIMx_IFR) (578)19.3.26中断标志清除寄存器(TIMx_ICLR) (580)19.3.27展频及中断触发选择(TIMx_CR) (581)19.3.28AOS选择控制寄存器(TIMx_AOSSR) (583)19.3.29AOS选择控制寄存器标志清除(TIMx_AOSCL) (584)19.3.30端口刹车控制寄存器(TIMx_PTBKS) (585)19.3.31端口触发控制寄存器(TIMx_TTRIG) (586)19.3.32AOS 触发控制寄存器(TIMx_ITRIG) (587)19.3.33端口刹车极性控制寄存器(TIMx_PTBKP) (588)20实时时钟(RTC) (589)20.1实时时钟简介 (589)20.2实时时钟功能描述 (591)20.2.1上电设定 (591)20.2.2RTC 计数开始设定 (591)20.2.3系统低功耗模式切换 (591)20.2.4读出计数寄存器 (592)20.2.5写入计数寄存器 (592)20.2.6闹钟设定 (593)20.2.71Hz 输出 (593)20.2.8时钟误差补偿 (594)20.3RTC 中断 (596)20.3.1RTC 闹钟中断 (596)20.3.2RTC 周期中断 (596)20.4RTC 寄存器描述 (597)20.4.1控制寄存器0(RTC_CR0) (598)20.4.2控制寄存器1(RTC_CR1) (600)20.4.3秒计数寄存器(RTC_SEC) (602)20.4.4分计数寄存器(RTC_MIN) (602)20.4.5时计数寄存器(RTC_HOUR) (603)20.4.6日计数寄存器(RTC_DAY) (605)20.4.7周计数寄存器(RTC_WEEK) (606)20.4.8月计数寄存器(RTC_MON) (607)20.4.9年计数寄存器(RTC_YEAR) (607)20.4.10分闹钟寄存器(RTC_ALMMIN) (608)20.4.11时闹钟寄存器(RTC_ALMHOUR) (608)20.4.12周闹钟寄存器(RTC_ALMWEEK) (609)20.4.13时钟误差补偿寄存器(RTC_COMPEN) (610)21看门狗定时器(WDT) (612)21.1WDT 简介 (612)21.2WDT 功能描述 (613)21.2.1WDT溢出后产生中断 (613)21.2.2WDT溢出后产生复位 (613)21.3WDT 寄存器描述 (615)21.3.1WDT 清除控制寄存器(WDT_RST) (615)21.3.2WDT_CON 寄存器 (616)22脉冲计数器(PCNT) (617)22.1脉冲计数器简介 (617)22.2脉冲计数器主要特性 (617)22.3脉冲计数器功能描述 (618)22.3.1整体框图 (618)22.3.2信号说明 (618)22.3.3计数模式 (619)22.3.3.1单通道脉冲计数模式(Single Mode) (619)22.3.3.2双通道非交脉冲计数模式(Dual Mode) (620)22.3.3.3双通道正交脉冲记数模式(Quad Mode) (621)22.3.4脉冲宽度滤波 (623)22.3.5超时 (623)22.4PCNT 寄存器描述 (624)22.4.1PCNT 启动寄存器(PCNT_RUN) (625)22.4.2PCNT 控制寄存器(PCNT_CTRL) (626)22.4.3PCNT 滤波控制寄存器(PCNT_FLT) (627)22.4.4PCNT 超时控制寄存器(PCNT_TOCR) (628)22.4.5PCNT 命令寄存器(PCNT_CMD) (629)22.4.6PCNT 状态寄存器1(PCNT_SR1) (630)22.4.7PCNT 计数寄存器(PCNT_CNT) (630)22.4.8PCNT 计数溢出寄存器(PCNT_TOP) (631)22.4.9PCNT 计数溢出缓存寄存器(PCNT_BUF) (631)22.4.10PCNT 中断标识寄存器(PCNT_IFR) (632)22.4.11PCNT 中断清除寄存器(PCNT_ICR) (633)22.4.12PCNT 中断使能寄存器(PCNT_IEN) (633)22.4.13PCNT 同步状态寄存器(PCNT_SR2) (634)23通用同步异步收发器(UART) (635)23.1概述 (635)23.2功能框图 (636)23.3工作模式 (637)23.3.1Mode0(同步模式,半双工) (637)23.3.1.1发送数据 (637)23.3.1.2接收数据 (637)23.3.2Mode1(异步模式,全双工) (638)23.3.2.1发送数据 (638)23.3.2.2接收数据 (639)23.3.3Mode2(异步模式,全双工) (639)23.3.3.1发送数据 (639)23.3.3.2接收数据 (640)23.3.4Mode3(异步模式,全双工) (640)23.3.4.1发送数据 (640)23.3.4.2接收数据 (641)23.4波特率编程 (642)23.4.1Mode0 (642)23.4.2Mode1/3 (642)23.4.3Mode2 (646)23.5传输数据结构 (647)23.6帧错误检测 (647)23.7多机通讯 (648)23.7.1自动地址识别 (648)23.7.2给定地址 (648)23.7.3广播地址 (649)23.7.4举例 (649)23.8DMAC硬件握手 (649)23.9硬件流控 (650)23.9.1nRTS流控 (650)23.9.2CTS流控 (650)23.10收发端缓存 (652)23.10.1接收缓存 (652)23.10.2发送缓存 (652)23.11寄存器 (654)23.11.1数据寄存器(UARTx_SBUF) (654)23.11.2控制寄存器(UARTx_SCON) (655)23.11.3地址寄存器(UARTx_SADDR) (657)23.11.4地址掩码寄存器(UARTx_SADEN) (657)23.11.5标志位寄存器(UARTx_ISR) (658)23.11.6标志位清除寄存器(UARTx_ICR) (659)23.11.7波特率寄存器(UARTx_SCNT) (659)24低功耗同步异步收发器(LPUART) (660)24.1概述 (660)24.2功能框图 (661)24.3配置时钟和传输时钟 (661)24.3.1配置时钟 (661)24.3.2传输时钟 (661)24.4工作模式 (662)24.4.1Mode0(同步模式,半双工) (662)24.4.1.1发送数据 (662)24.4.1.2接收数据 (662)24.4.2Mode1(异步模式,全双工) (663)24.4.2.1发送数据 (663)24.4.2.2接收数据 (663)24.4.3Mode2(异步模式,全双工) (664)24.4.3.1发送数据 (664)24.4.3.2接收数据 (664)24.4.4Mode3(异步模式,全双工) (665)24.4.4.1发送数据 (665)24.4.4.2接收数据 (665)24.5.1Mode0 (667)24.5.2Mode1/3 (667)24.5.3Mode2 (667)24.6传输数据结构 (671)24.7帧错误检测 (672)24.8多机通讯 (672)24.8.1自动地址识别 (672)24.8.2给定地址 (673)24.8.3广播地址 (673)24.8.4举例 (673)24.9DMAC硬件握手 (674)24.10硬件流控 (674)24.10.1nRTS流控 (675)24.10.2CTS流控 (676)24.11收发端缓存 (677)24.11.1接收缓存 (677)24.11.2发送缓存 (678)24.12寄存器 (679)24.12.1数据寄存器(LPUARTx_SBUF) (679)24.12.2控制寄存器(LPUARTx_SCON) (680)24.12.3地址寄存器(LPUARTx_SADDR) (682)24.12.4地址掩码寄存器(LPUARTx_SADEN) (682)24.12.5标志位寄存器(LPUARTx_ISR) (683)24.12.6标志位清除寄存器(LPUARTx_ICR) (684)24.12.7波特率寄存器(LPUARTx_SCNT) (684)25循环冗余校验(CRC) (685)25.1概述 (685)25.2功能框图 (685)25.3功能描述 (685)25.4寄存器 (686)25.4.1控制寄存器(CRC_CR) (686)25.4.2结果寄存器(CRC_RESULT) (687)25.4.3数据寄存器(CRC_DA TA) (687)25.5软件基本操作 (689)25.5.1CRC16编码模式 (689)25.5.2CRC16检验模式 (689)25.5.3CRC32编码模式 (689)25.5.4CRC32检验模式 (690)26真随机数发生器(TRNG) (691)26.1概述 (691)26.2功能框图 (691)26.4寄存器 (692)26.4.1控制寄存器(TRNG_CR) (692)26.4.2模式寄存器(TRNG_MODE) (693)26.4.3数据寄存器0(TRNG_DA TA0) (694)26.4.4数据寄存器1(TRNG_DA TA1) (694)26.5软件基本操作 (695)26.5.1生成64bits真随机数的操作流程(上电第一次) (695)26.5.2生成64bits真随机数的操作流程(非上电第一次生成) (696)27高级加密标准模块(AES) (697)27.1功能定义 (697)27.1.1AES算法简述 (697)27.1.2AES模块功能描述 (699)27.2模块寄存器说明 (700)27.2.1控制寄存器(AES_CR) (700)27.2.2数据寄存器(AES_Data) (701)27.2.3密钥寄存器(AES_Key) (702)27.3异常机制 (703)27.4本模块操作说明 (704)27.4.1IP操作的共同点 (704)27.4.2加密操作流程 (704)27.4.3解密操作流程 (704)27.4.4数据示例 (705)27.5运行时间说明 (706)28液晶控制器(LCD) (707)28.1LCD简介 (707)28.2LCD主要特性 (707)28.3LCD框图 (708)28.4LCD驱动波形 (709)28.4.1静态驱动波形 (709)28.4.21/2Duty 1/2Bias驱动波形 (710)28.4.31/2Duty 1/3Bias驱动波形 (711)28.4.41/3Duty 1/2Bias驱动波形 (712)28.4.51/3Buty 1/3Bias驱动波形 (713)28.4.61/4Duty 1/2Bias驱动波形 (714)28.4.71/4Duty 1/3Bias驱动波形 (715)28.4.81/6Duty 1/3Bias驱动波形 (716)28.4.91/8Duty 1/3Bias驱动波形 (717)28.5LCD Bias产生电路 (718)28.5.1内部电阻模式 (718)28.5.2外部电容模式 (719)28.5.3外部电阻模式 (720)28.7中断 (721)28.8LCD 显示模式 (721)28.8.1LCD 显示模式1 (MODE = 1) (722)28.8.2LCD 显示模式0 (MODE = 0) (723)28.9LCD 寄存器 (724)28.9.1配置寄存器0(LCD_CR0) (725)28.9.2配置寄存器1(LCD_CR1) (727)28.9.3中断清除寄存器(LCD_INTCLR) (728)28.9.4输出配置寄存器0(LCD_POEN0) (728)28.9.5输出配置寄存器1(LCD_POEN1) (729)28.9.6LCD_RAM0~7 (731)28.9.7LCD_RAM8~F (732)29模数转换器(ADC) (733)29.1模块简介 (733)29.2ADC框图 (734)29.3转换时序及转换速度 (735)29.4单次转换模式 (736)29.5扫描转换模式 (738)29.5.1顺序扫描转换模式 (738)29.5.2插队扫描转换模式 (740)29.5.3扫描转换触发DMA读取 (744)29.6连续转换累加模式 (745)29.7ADC转换外部触发源 (748)29.8ADC转换结果比较 (749)29.9ADC中断 (750)29.10使用温度传感器测量环境温度 (751)29.11ADC 模块寄存器 (753)29.11.1ADC 基本配置寄存器0(ADC_CR0) (755)29.11.2ADC 基本配置寄存器1(ADC_CR1) (757)29.11.3ADC 顺序扫描转换通道配置寄存器0(ADC_SQR0) (759)29.11.4ADC 顺序扫描转换通道配置寄存器1(ADC_SQR1) (760)29.11.5ADC 顺序扫描转换通道配置寄存器2(ADC_SQR2) (761)29.11.6ADC 插队扫描转换通道配置寄存器(ADC_JQR) (762)29.11.7ADC 顺序扫描转换通道x转换结果(ADC_SqrResult0 - 15) (762)29.11.8ADC 插队扫描转换通道x转换结果(ADC_JqrResult0 - 3) (763)29.11.9ADC 转换结果(ADC_Result) (763)29.11.10A DC 转换结果累加值(ADC_ResultAcc) (764)29.11.11ADC 比较上阈值(ADC_HT) (764)29.11.12A DC 比较下阈值(ADC_LT) (765)29.11.13A DC 中断标志寄存器(ADC_IFR) (766)29.11.14A DC 中断清除寄存器(ADC_ICR) (767)29.11.15A DC 单次转换或顺序扫描转换外部中断触发源配置寄存器(ADC_ExtTrigger0) (768)29.11.16A DC 插队扫描转换外部中断触发源配置寄存器(ADC_ExtTrigger1) (770)29.11.17A DC 单次转换启动控制寄存器(ADC_SglStart) (772)29.11.18A DC 顺序扫描转换启动控制寄存器(ADC_SqrStart) (772)29.11.19A DC 插队扫描转换启动控制寄存器(ADC_JqrStart) (773)30模拟比较器(VC) (774)30.1模拟电压比较器VC 简介 (774)30.2电压比较器框架图 (775)30.3建立/响应时间 (775)30.4滤波时间 (776)30.5迟滞功能 (776)30.6VC 寄存器 (777)30.6.1VC 配置寄存器(VC_CR) (778)30.6.2VC0 配置寄存器(VC0_CR) (780)30.6.3VC1 配置寄存器(VC1_CR) (782)30.6.4VC0 输出配置寄存器(VC0_OUT_CFG) (784)30.6.5VC1 输出配置寄存器(VC1_ OUT_CFG) (786)30.6.6VC 中断寄存器(VC_IFR) (788)31低电压检测器(LVD) (789)31.1LVD 简介 (789)31.2LVD 框图 (789)31.3迟滞功能 (790)31.4数字滤波 (790)31.5配置示例 (791)31.5.1LVD配置为低电压复位 (791)31.5.2LVD配置为电压变化中断 (791)31.6LVD寄存器 (792)31.6.1LVD 配置寄存器(LVD_CR) (792)31.6.2LVD 中断寄存器(LVD_IFR) (794)32运算放大器(OPA) (795)32.1OPA 特性 (795)32.2OPA 功能描述 (796)32.2.1PGA功能 (796)32.2.2运放功能 (796)32.3配置 (797)32.3.1PGA增益 (797)32.3.2单位增益PGA (798)32.3.3正向输入PGA (798)32.3.4反向输入PGA (799)32.3.5级联反向输入PGA (800)32.3.6级联正向输入PGA (801)32.3.7两运放差分PGA (802)32.4OPA寄存器 (804)32.4.1OPA 配置寄存器(OPA_CR0) (805)32.4.2OPA 配置寄存器(OPA_CR1) (807)32.4.3OPA 配置寄存器(OPA_CR2) (809)33模拟其它寄存器 (811)33.1BGR 配置寄存器(BGR_CR) (811)34SWD 调试接口 (812)34.1SWD 调试附加功能 (812)34.2ARM® 参考文档 (813)34.3调试端口引脚 (814)34.3.1SWD 端口引脚 (814)34.3.2SW-DP 引脚分配 (814)34.3.3SWD 引脚上的内部上拉 (814)34.4SWD 端口 (815)34.4.1SWD协议简介 (815)34.4.2SWD 协议序列 (815)34.4.3SW-DP 状态机(复位、空闲状态、ID 代码) (816)34.4.4DP 和AP 读/写访问 (816)34.4.5SW-DP 寄存器 (817)34.4.6SW-AP 寄存器 (818)34.5内核调试 (819)34.6BPU(断点单元) (819)34.6.1BPU 功能 (819)34.7DWT(数据观察点) (820)34.7.1DWT 功能 (820)34.7.2DWT 程序计数器采样寄存器 (820)34.8MCU 调试组件(DBG) (821)34.8.1对低功耗模式的调试支持 (821)34.8.2对定时器、看门狗的调试支持 (821)34.9调试模式模块工作状态控制(DEBUG_ACTIVE) (822)35电气特性 (824)35.1测试条件 (824)35.1.1最小和最大数值 (824)35.1.2典型数值 (824)35.1.3供电方案 (825)35.2绝对最大额定值 (826)35.3工作条件 (828)35.3.1通用工作条件 (828)35.3.2上电和掉电时的工作条件 (828)35.3.3内嵌复位和LVD模块特性 (829)35.3.4内置的参考电压 (831)35.3.6从低功耗模式唤醒的时间 (835)35.3.7外部时钟源特性 (836)35.3.7.1外部输入高速时钟 (836)35.3.7.2外部输入低速时钟 (836)35.3.7.3高速外部时钟XTH (837)35.3.7.4低速外部时钟XTL (838)35.3.8内部时钟源特性 (840)35.3.8.1内部RCH振荡器 (840)35.3.8.2内部RCL振荡器 (840)35.3.9PLL特性 (841)35.3.10存储器特性 (841)35.3.11EFT特性 (841)35.3.12ESD特性 (842)35.3.13I/O端口特性 (842)35.3.13.1输出特性——端口 (842)35.3.13.2输入特性——端口PA,PB,PC,PD, RESET (843)35.3.13.3端口外部输入采样要求——Timer Gate/Timer Clock (844)35.3.13.4端口漏电特性——PA,PB,PC,PD (844)35.3.14RESETB引脚特性 (845)35.3.15ADC特性 (845)35.3.16VC特性 (848)35.3.17OPA特性 (848)35.3.18LCD控制器 (850)36唯一设备ID 寄存器(80 位) (851)37封装尺寸 (852)38附录A SysTick 定时器 (857)38.1SysTick 定时器简介 (857)38.2设置SysTick (857)38.3SysTick 寄存器 (858)38.3.1SysTick 控制和状态寄存器(CTRL) (858)38.3.2SysTick 重载寄存器(LOAD) (858)38.3.3SysTick 当前值寄存器(V AL) (858)38.3.4SysTick 校准值寄存器(CALIB) (859)39附录B 文档约定 (860)39.1寄存器相关缩写词列表 (860)39.2词汇表 (860)版本记录& 联系方式 (861)。
VAISALA GMD20 User 说明书
CO2 transmitter GMD20 and GMD20D
M210292en-A
POWER SUPPLY REQUIREMENTS
The GMD20 transmitter is designed to operate from a nominal 24 VAC/VDC supply. The power supply should maintain the voltage between 18...30 VDC or 20...26 VAC for all load conditions and all mains voltages. The power input includes a halfwave rectifier. To avoid current peaks, it is recommended to use a DC supply. The average transmitter current consumption is 85 mA maximum but peak currents of 170 mA may occur during normal operation.
A)
24VAC
GM20
Supply voltage
24V
OUT
GND
24VAC
Supply voltage
GM20
24V
OUT
GND
CONTROLLER
Signal output
Signal output
B)
24VAC Supply voltage
Supply voltage
GM20
24V
OUT
GND
MOUNTING
CIRRUS SR20 飞行手册说明书
Seats…………………………...ADJUSTED & LOCKED Seat Belts and Harnesses……………...….….SECURE Doors…...CLOSED and CHECKED (may be deferred) Key………………………………………......IN IGNITION Brakes………………………………...…………….HOLD BAT Master Switches….…………....ON (Check Volts) Strobe Lights…………………………………………..ON Mixture……………………………….……….FULL RICHPitot heat…………………….……...………..ONNavigation Lights…………….…...…...…….ONLanding Lights…………………………….....ONAnnunciator Lights……………………..CHECK Amp Meter Indication………….…....CHECK POSITIVE Pitot Heat…………………….…………..AS REQUIRED Navigation Lights………………………..AS REQUIRED Landing Light………………..…………..AS REQUIRED Magnetos……………………...………….CHECK BOTH Ignition Switch…....R, check RPM, then BOTHIgnition Switch…....L, check RPM, then BOTH Engine Parameters………………….……..…….CHECK Power Lever…………………………………...1000 RPM Autopilot………….…….......TEST, then DISCONNECT Flight Instruments…………………….....CHECK & SET Heading Bug………….....RUNWAY HEADINGAltitude Bug…………….….INITIAL ALTITUDEVSI Setting…..………CLIMB RATE DESIRED Trim……..…..SET IN T/O RANGE (aileron & elevator) Flight Controls………………...…...FREE & CORRECT Doors……….............…..……CLOSED and CHECKED Determine Need for/Direction of Crosswind Correction Type of Takeoff Planned (Normal, Soft, Short) Direction of Departure or Initial Assigned Heading Initial Planned or Assigned AltitudeRotation Speed is 65-70 KIASBEFORE TAKEOFF BRIEFINGNORMAL CHECKLISTPower Lever…………………………..FULL FORWARD Engine Instruments……………………………...CHECK Brakes………………………………………….RELEASE Elevator Control…...ROTATE Smoothly at 65-70 KIAS At 85 KIAS, Flaps……………………………….…….UP Initial Climb………………………….……..…....96 KIASFlaps…………………………………………………..50% Brakes……………………………………………....HOLD Power Lever………………….……….FULL FORWARD Engine Instruments………………………….…..CHECK Brakes………………………………………….RELEASE Elevator Control…….……Rotate Smoothly at 65 KIAS Airspeed at Obstacle…………………..………..77 KIAS Transition to Normal Climb….…….……..….....96 KIASEnroute Climb…………………………...……..105 KIAS Throttle………………………….…………...FULL OPEN Mixture…………………………………..……FULL RICH Engine Parameters…………………………...….CHECK Fuel Pump…………………………………………….OFF Landing Light..........................................................OFF Cruise Power…………………...……..SET 55% to 75% Mixture………………......................…………SEE QRC Engine Parameters………………..………….MONITOR Fuel Flow and Balance………………….…...MONITOR COM 2……………………………………..Monitor 121.5Note: The Fuel Pump must be used for switching from one tank to another to avoid engine restart delays should engine quit due to fuel starvation.Cruise Leaning if Desired:Best Power = 75° Rich of Peak EGT75% Power or LessBest Economy = 50° Lean of Peak EGT65% Power or LessApproach Settings: MP KIAS FLAPSPrior to FAF: 22 100 50% Glideslope: 12 100 50%NP Decent: 10 100 50% ATIS/AWOS/Local Weather..………………RECEIVED Approach Briefing……………….………….COMPLETE Altimeter...…………………………………………….SET Cabin Heat/Defrost……………....……..AS REQUIRED Landing Light………….……………………………….ON Fuel System…………………...………………….CHECK Mixture…………………………………...AS REQUIRED Brake Pressure……….………………………….CHECK Seat Belts and Harnesses………………...…..SECURE Fuel Pump……………………………………......BOOST Mixture………………………….…………….FULL RICH Flaps…………………………………......AS REQUIRED Autopilot……………………......OFF BELOW 500’ AGLDownwind………………...…….100 KIAS, FLAPS 50% Base………………………...…..90 KIAS, FLAPS 100% Final Approach……….……….*80 KIAS, FLAPS 100% Touchdown………………….…..MAIN WHEELS FIRST Nosewheel………………………..…..GENTLY LOWER Braking…………………...……...MINIMUM REQUIRED * Airspeed on final approach should be increased at least 5 KIAS in turbulent conditions.Power Lever……………………………….….1000 RPM Fuel Pump…………..………………………………..OFF Wing Flaps…………..………………………………....UP Transponder…………………………………...…...STBY Lights…………………………...………..AS REQUIRED Mixture……………………………….……………..LEAN Pitot Heat………………………..…………………...OFF Fuel Pump……………………………..……………..OFF Throttle……………………….………………………IDLE Ignition Switch…………………..CHECK GROUNDING Avionics Power Switch….…………………………...OFF Mixture……………………………..……..IDLE CUTOFF All Switches (right to left).....…….……………….....OFF Magnetos…...………..………….…………….……..OFF ELT………………………….....TRANSMIT LIGHT OUT CAPS Pin………………………………………..INSTALL Chocks, Tie-Downs, Pitot Cover.……...AS REQUIRED Brake Sensors……………………………...….INSPECTNORMAL TAKEOFF CRUISE CHECKARRIVAL AREA CHECK BEFORE LANDING CHECK AFTER LANDING CHECK SHUTDOWN CHECKNORMAL LANDINGPAGE 2SHORT FIELD TAKEOFF CLIMB CHECK (above 1000 AGL)Wing Flaps………...……………………..………...100% Airspeed……….....MAINTAIN 75 KIAS UNTIL FLARE Trim……………………………………….……..ADJUST Power……………E TO CONTROL GLIDE PATH Clear of Obstacles………SLOWLY REDUCE POWER Attitude………..NOSE DOWN TO MAINTAIN 75 KIAS Touchdown……………………..MAIN WHEELS FIRST Brakes………………………….….APPLY AS NEEDED Wing Flaps..RETRACT (improves brake effectiveness)Power should slowly be reduced once clear of obstacles, reaching idle just prior to touchdown.Do NOT lock-up the brakes as this will flat spot the tires and increase the stopping distance.Power Lever……………………...SET 65-75% POWER Fuel Pump…………………………..……...VERIFY OFF Lean Assist........................................PRESS BUTTONBEST POWER: Lean until “Peak Detected” thenslowly enrich the mixture until “Peak Detected (Rich)” shows. “Best Power” will display at optimal mixture.BEST ECONOMY: Use 65% or less power for BEST ECONOMY settingsLean until “Last Peak Detected” is shown. Continue leaning until “Best Economy” is shown.Press the “Normalize” button after leaning the mixture.Oil Type Used………….…AEROSHELL OIL W 15w50 Oil Quantity (Normal)………………...MINIMUM 6 QTS. Oil Quantity (Long-Distance)…………………….7 QTS. Fuel at Tabs……………………….26 GALS. USEABLE Fuel to Top………………...………56 GALS. USEABLE Nose Tire Pressure………………………...40 +2/-0 PSI Main Tire Pressure………………………....53 +2/-0 PSIThree rows of circuit breakers are located near the pilots right leg. This checklist series describes them by row(F ront, C enter, A ft ) and number from the top down (1-13).EXAMPLE: F4 is Front row, 4th breaker from the top. AWOS/ATIS………………...………………..OBTAINED Altimeter………..……………….…………………....SET Localizer / VOR / NDB Frequency…………………SET Approach Course…………………………………….SET Runway Length (Rwy ldg)……………...………...NOTE Touchdown Zone Elevation (TDZ)….…………...NOTE Airport Elevation…………………………………...NOTE Approach Lighting……………………………...….NOTE Missed Approach Procedure……….………….REVIEW Approach Control Frequency………….……………SET Tower Frequency…………..……….SET IN STANDBY Minimum Safe Altitude in Sector……………...….NOTE MDA/DH (Minimums)……………….……..BUG (if able) Missed Approach Point (MAP)…………...DETERMINE Direction of Turn Off Runway After Landing…....NOTENote: For a non-precision approach determine how the Missed Approach Point will be identified, either using timing or DME distance as published.Instrument Approach……..…....105 KIAS/FLAPS 50% Downwind………………….….…100 KIAS/FLAPS 50% Base…………………………..….90 KIAS/FLAPS 100% Final………………..…...……....*80 KIAS/FLAPS 100%*Reduce airspeed to 75 KIAS on short final. Use 85-90 KIAS for No Flap Landing.Approach Settings: MP KIAS FLAPSPrior to FAF: 17 100 50% Glideslope: 12 100 50% NP Decent:10 100 50%V SPEEDSVne / Never Exceed……………………...……200 KIAS Vno / Maximum Structural Cruise….....…...…165 KIAS Vo / Operating Maneuvering. (3000 lbs.).....131 KIAS Vfe / Max. Speed w/flaps 50%.……........…..120 KIAS Vfe / Max. Speed w/Flaps 100%…………….100 KIAS Vpd / Max. Demo’d Chute Deployment….…..135 KIAS Vy / Best Rate of Climb………….….………...96 KIAS Vx / Best Angle of Climb………………….…...81 KIAS Vr / Rotate…………………….………….……..67 KIAS Vs1 / Stall in Cruise Configuration………...…..65 KIAS Vso / Stall in Landing Configuration……….…..56 KIASNormal Climbout……………….....…………..…96 KIAS Enroute Climb…………………..…..………….105 KIAS Best Glide (at 3000 lbs.)………….……..……...96 KIASSHORT-FIELD LANDINGINSTRUMENT APPROACHRECOMMENDED AIRSPEEDSCRUISE LEANINGThe POH remains the official source of information.SERVICING CIRCUIT BREAKERS CIRRUS SR20 QUICK REFERENCE CARDQRCBRIEFALT 1 LIGHT STEADYVERIFY CONDITION: Prior to conducting the following procedure verify that ALT 1 is offline by checking the voltage meter indication for ALT 1. If the indication is near 28 volts the problem is a bad ALT 1 current sensor and you should NOT proceed with the following procedure.If ALT 1 Current is Near 24 VoltsALT 1 Master Switch………………………………...OFF ALT 1 Circuit Breaker (C5)………..CHECK and RESET ALT 1 Master Switch………………………………….ONIf alternator does not resetALT 1 Master Switch………………………………...OFF Autopilot…………………………………….…..ENGAGEReduce LoadsAudio Panel………………………….………………...OFF GPS/COM 2……………………….……….………….OFF Fuel Pump………………………….….……………...OFF Panel and Overhead Lights…….…………………...OFF Landing Light………………….………………………OFF Strobe Lights……….……………………….………...OFF Pitot Heat……..…………………………………….....OFFPull Circuit BreakersSkywatch/TAWS (F1)….……………..……………..PULL WX/Stormscope (F5)……………………………......PULL MFD (F6).……………………………………...……..PULL Use the Autopilot to fly the aircraft.Avoid use of manual trim.Do NOT reset a circuit breaker more than one time. Land within ONE hour. Plan on a flaps up or flaps 50% landing. Do NOT extend flaps to 100% for landing. You may not have sufficient power to retract flaps should a go-around be necessary.NOTE: ALT 2 will not come on line at low RPM settings.VERIFY CONDITION: Prior to conducting the following procedure verify that ALT 2 is offline by checking the voltage meter indication for ALT 2. If the indication is higher than the ALT 1 voltage then the problem is a bad ALT 2 current sensor and you should NOT proceed with the following procedure.If ALT 2 Voltage is the Same as ALT 1 Voltage ALT 2 Master Switch………………………..………..OFF Discontinue IFR Flight as soon as practical. Redundant electrical power is no longer available. 1. Prime engine until 15 GPH is obtained:- Power Lever FULL FORWARD- Mixture FULL FORWARD- Boost pump switch to PRIME2. Follow quickly with MIXTURE IDLE CUTOFF(power lever remains full forward).3. Boost pump switch to BOOST.4. Clear prop and START engine.5. If no start within 15 seconds repeat procedure butturn OFF boost pump after priming.6. At engine start RETARD POWER LEVERfollowed by FULL RICH mixture.7. Lean mixture as required. Airspeed…………………..….REDUCE TO 80-90 KIAS Flaps………………………………………….…SET 50% Land………………………...AS SOON AS PRACTICALNOTE: With electrical failure the audio panel connects COM 1 to the pilot’s headset and speakers . Switches, Controls……………………………….CHECK Frequency……………………………………....CHANGE Circuit Breakers…………………………….…….CHECK Headset…………CHECK CONNECTIONS / CHANGE Hand Held Microphone………………………CONNECT Transponder……………………………...….CODE 7600 Any trim or autopilot failure can be overridden by use of the control yoke.Airplane Control……………………………..MANUALLY Autopilot…………………………………....DISENGAGE If Problem Not Corrected:Circuit Breakers…………….…....PULL AS REQUIRED PITCH TRIM (F11)ROLL TRIM (F12)AUTOPILOT (A9)Power Lever……………………………..AS REQUIRED Control Yoke………....MANUALLY HOLD PRESSURE Circuit Breaker (A1)………………...PULL AND RESETHOT STARTCIRRUS SR20 ABNORMAL PROCEDURES ADDITIONAL ABNORMAL PROCEDURES ARE LOCATED IN THE PILOT’S OPERATING HANDBOOKALT 2 LIGHT STEADYDOOR OPEN IN FLIGHT COMMUNICATIONS FAILURETRIM / AUTOPILOT FAILURE ENGINE INSTRUMENTS RESETEMERGENCY CHECKLISTFLY THE AIRPLANE - IDENTIFY EMERGENCY - READ CHECKLIST - DO NOT HURRY!ENGINE FAILURE DURING TAKEOFF ROLL Throttle……..………………..……………..IDLE Brakes…..…………...…………..………APPLY Wing Flaps…..……...…...…………...RETRACT Mixture……………………...….............CUTOFF Master Switch……………...………….….....OFF IMMEDIATELY AFTER LIFTOFFBest Glide or Landing Speed.…ESTABLISH Mixture………………..…...…....IDLE CUTOFF Fuel Selector Valve…..……ROTATE TO OFF Ignition Switch…….……………………....OFF Wing Flaps..…….……..……...AS REQUIRED If time permits:Power Lever……………………….……….IDLE Fuel Pump…………………………...……...OFF Bat-Alt Master Switches……………….…..OFF Seat Belts……………......ENSURE SECURED DURING FLIGHT (ATTEMPT RESTART) Airspeed……………….……….………96 KIAS Mixture………….….…..…………………..RICH Fuel Selector Valve….……..SWITCH TANKS Fuel Pump…………..………….....…...BOOST Alternate Air…………………………..…......ON Ignition……………………………….…….BOTH WITHOUT ENGINE POWER Airspeed………..……..…...96 KIAS (flaps up) Radio……………..……..TRANSMIT MAYDAY Transponder……..…………...SQUAWK 7700 If off airport………..…...……..ACTIVATE ELT Power Lever……...………….…………….IDLE Mixture…………..……...……………..CUTOFF Fuel Selector Valve……..…ROTATE TO OFF Ignition Switch………..…………………....OFF Fuel Pump…………………………...……...OFF Flaps (when landing assured)…………...100% Master Switch……….………………..……..OFF Seatbelts…………………………….....SECURE Exit Aircraft……………….MEET PAX UPWINDPRECAUTIONARY LANDING WITH ENGINE POWER (off-field) Seatbelts……………………………...SECURE Flaps……………….…………….…………50% Airspeed……………...………………..95 KIAS Selected Field.…...FLY OVER TO OBSERVE Selected Field……….….LINE UP FOR FINAL Avionics Power Switch…….……………...OFF Wing Flaps……..….………………...……100% Airspeed………….………..…………...75 KIAS Master Switch….……..…………………….OFF Doors...UNLATCH PRIOR TO TOUCHDOWN Touchdown………….....SLIGHTLY TAIL LOW Ignition Switch……...……………………....OFF Brakes…………………….….APPLY HEAVILY IN FLIGHT Mixture…………..……………………CUTOFF Fuel Pump……………………...………….OFF Power Lever………………………….…...IDLE Airflow Selector......................................OFF Fuel Selector....….………..ROTATE TO OFF Ignition……………………………………...OFF Cabin Door...................OPEN RIGHT DOOR If fire fails to extinguish increase glide speed to incombustible mixture speed.Emergency Landing ………...….….EXECUTE DURING START Mixture……………..…………..IDLE CUTOFF Fuel Pump….……………………………...OFF Fuel Selector……………………...…...….OFF Power Lever..………………….....FORWARD Starter……………………………..…...CRANK Fire Extinguisher…....……OBTAIN AND USE If flames persist:Power Lever………………………..……...IDLE Fuel Pump……………………………….....OFF Mixture………………………………...CUTOFF Fuel Selector……………………………….OFF Ignition Switch……………………………...OFF Bat-Alt Master Switches…………………..OFF Exit Aircraft…….……….MEET PAX UPWINDENGINE FIREEMERGENCY LANDINGSR20PAGE 1IMMEDIATE ACTION ITEMS ARE IN BOLD PRINTRevision Date: 06 JUN 14EMERGENCY CHECKLISTFLY THE AIRPLANE - IDENTIFY EMERGENCY - READ CHECKLIST - DO NOT HURRY!CABIN FIREIN FLIGHTBat-Alt Master Switch…....……………….OFF Vents/Cabin Air/Heater.………….…CLOSED Fire Extinguisher…………..………ACTIVATEWARNING: Ventilate cabin by opening vents and opening doors if needed after use of fire extinguisher.Avionics Power Switch………...…….……..OFF All Other Switches (except ignition)….…...OFFIf fire appears to be out and electrical power is required for continued safe flight (IFR flight): Bat-Alt Master Switch…..………………..….ON Circuit Breakers…....CHECK for faulty circuit DO NOT RESET if breaker has tripped. Individual Radio Switches..…………..……OFF Avionics Power Switch……….……………..ON GPS-COM/Electrical Switches…..ON one at a time until the short circuit is localized.Pitot Heat Switch……………………….….OFF Navigation Light Switch……………..…...OFF Landing Light Switch...............................OFF Strobe Light Switch……………………….OFFPerform a sideslip to keep flames away from fuel tank and cabin.Putting the airplane into a dive may blow out the fire. Do not exceed Vne (200) during the dive.Land ASAP using wing flaps only as required for final approach and touchdown.WING FIRE Pitot Heat Switch……..…………………...ON Time……………………………...……..NOTED Heading and/or Altitude………......CHANGE A heading change of 180° should return you to ice free conditions. Lower altitudes are normally warmer. Advise ATC if under IFR control.Cabin Heat………………………....MAXIMUM Windshield Defrost……….…….FULL OPEN Alternate Induction Air…………………....ONWARNING: With extremely rapid ice buildup select a suitable off-airport landing site.Stall Speed will be significantly higher with ice accretion of 1/4 inch or more.Wing Flaps Use flaps 50% or no flaps as wing wake airflow change with flaps down could result in loss of elevator effectiveness.Forward Slip to land if needed for improved forward visibility.Approach : If ice is suspected to be adhering to the tail use higher approach speeds.No-Flap use 95-100 KIAS Flaps 50% use 90-95 KIASLand in a level attitude.SEE POH SECTION 3This checklist was created to deal with most, but not all, emergency situations. Additional informa-tion is available in Section 3 of the Pilot Operating Handbook (POH). The POH is the definitive source of information concerning operation of this aircraft. The Pilot in Command is responsible for complying with all items in the POH and applicable STC’s.ICING ENCOUNTERPAGE 2OTHER EMERGENCIES SR20Copyright SafeAviator, 2014IMMEDIATE ACTION ITEMS ARE IN BOLD PRINT。
塞拉斯 sr20飞机系统手册说明书
CIRRUS SR20 AIRCRAFT SYSTEMS1.GENERALa.Enginesi.Number of Engines: 1ii.Number of Cylinders: 6iii.Engine Manufacturer: Teledyne Continentaliv.Engine Model Number: IO-360-ESv.Fuel Metering: Fuel Injectedvi.Engine Cooling: Air Cooledvii.Engine Type: Horizontally Opposed, Direct Driveviii.Horsepower Rating: 200 HP @ 2700 RPMb.Propellersi.Number of Propellers: 1ii.Propeller Manufacturer: Hartzelliii.Propeller Type: Constant Speediv.Number of Blades: 2 or 3v.Propeller Diameter (2 blade): 76.0” (74.5” Minimum)vi.Propeller Diameter (3 blade): 74.0” (72.5” Minimum)c.Fueli.Fuel Capacity (U.S. gal.): 58.5able Fuel (U.S. gal.): 56.0iii.Fuel Grade, Aviation1.Minimum Octane: 100/130 – Green; 100LL Blued.Oili.Oil Capacity (U.S. qts.) 8e.Maximum W eightsi.Max. Takeoff Weight (lb.): 3050ii.Max. Landing Weight (lb.): 3050iii.Max. Weights in Baggage Compartment: 130iv.Full Fuel Payload (lb.): 622f.Standard Airplane W eightsi.Standard Empty Weight (lb.): 20501.Weight of a standard airplane including unusable fuel, full operating fluids, and fulloilii.Maximum Useful Load (lb.): 9501.The difference between the Maximum Takeoff Weight and the Standard EmptyWeight2.LIMITATIONSa.Airspeed Limitations (KIAS)i.V R : 66ii.V APP : 77iii.V CLB : 96iv.V50’ : 77v.V GLD : 99vi.V X : 83vii.V Y : 96viii.V SO : 61ix.V S1 : 69x.V FE : 104 (100%), 119 (50%)xi.V NO : 163xii.V A : 110-130xiii.V NE : 200b.Pow er Plant Limitationsi.Engine Manufacturer: Teledyne Continentalii.Engine Model Number: IO-360-ESiii.Power Rating: 200 HP @ 2700 RPMiv.Maximum RPM: 2700v.Oil Temperature: 240°F (115°C) maximumvi.Oil Pressure:1.Minimum: 10 PSI2.Maximum: 100 PSIc.Flight Load Factor Limits (Max Gross Weight)i.Flaps 0%: +3.8G, -1.9Gii.Flaps 50%: +1.9G, -0Giii.Flaps 100%: +1.9G, -0Gd.Types of Operationsi.VFR: Day, Nightii.IFR: Day, Nighte.Fuel Limitationsi.Total Capacity: 58.5 U.S. GAL.ii.Total Capacity Each Tank: 29.3 U.S. GAL.iii.Total Usable Fuel: 56.0 U.S. GAL.1.The usable fuel in this airplane has been determined as 28 gallons in each wingtankiv.Unusable Fuel 2.5 U.S. GAL.1.The unusable fuel for this airplane has been determined as 1.25 gallons in eachwing tank in critical flight attitudes3.AIRFRAME – see Cirrus Manual (7-6)a. A composite roll cage within the fuselage structure provides roll protection for the cabinoccupantsb.The avionics bay is located aft of bulkhead 222 (behind rear baggage compartment)c.Wings each contain a 29.3 gallon fuel tankd.Wings are attached to the fuselage through a spar carry-through located under the two frontseats4.FLIGHT CONTROLS – see Cirrus Manual (7-8)a.The flight controls use a normal cable, pulley and bell-crank system to connect the control stick tothe elevator and aileron.b.Pitch Trimi.Pitch Trim system does not move a trim tab. An electric motor moves the flight control toa desired position and keeps it there by changing the tension on a spring cartridge. Simplyput, the electric motor adjusts the tension on a spring that holds the flight control in adesired setting (i.e. for takeoff, spring loaded to Takeoff position). The moving of theflight control in turn moves the control stick.ii.In the event of a elevator control failure, you can use the elevator trim to control the pitch of the aircraft (so long as the elevator is not jammed)iii.Elevator (pitch) trim is pow ered by 28 VDC supplied through the 2-amp PITCH TRIM circuit breaker on ESS BUS 2c.Roll Trimi.Roll Trim operates the same way as the Pitch Trim systemii.Aileron trim is pow ered by 28 VDC supplied through the 2-amp ROLL TRIM circuit breaker on ESS BUS 2d.This aircraft is not equipped with control locks or gust locks, the trim spring cartridges havesufficient power to overcome any wind gust5.INSTRUMENT PANEL – see Cirrus Manual (7-14)a.The left display is called the Primary Flight Display (PFD) and displays the most critical flight datab.The right display is called the Multi Functional Display (MFD) and displays additional engine data,navigation, checklists, etc.c.Attitude Indicatori.The Primary Attitude Indicator information is presented on the PFD. Information isprovided by the Attitude and Heading Reference System (AHRS)ii.The Standby Attitude Indicator is electrically powered. A red GYRO flag indicates loss of electrical poweriii.The Standby Attitude Indicator is pow ered by 28 VDC and is supplied through the 5-amp STDBY ATTD 1 circuit breaker on the ESS BUS 1 and the 5-ampSTDBY ATTD 2 circuit breaker on the MAIN BUS 1d.Airspeed Indicatori.Primary airspeed data is provided by the Air Data Computer and is displayed on the PFD.Speed starts being displayed at 20 knotse.Altimeteri.Primary altitude data is provided by the Air Data Computer and is displayed on the PFD.The Altitude Reference Bug can be set using the “ALT SEL” knob on the FMS panel.f.Horizontal Situation Indicatori.Displayed on PFD; heading data is provided by the Attitude and Heading ReferenceSystem (AHRS) and the onboard magnetometersii.The HSI heading reference bug is set using the heading selection knob on the FMS keyboardg.Vertical Speed Indicatori.Displayed on PFD; data is provided by the Air Data Computer. Rate must exceed 100 feetper minute to be displayedh.Flight Instruments Review:i.Air Data Computer: Airspeed Indicator, Altimeter, Vertical Speed Indicatorii.Attitude and Heading Reference System (AHRS): Primary Attitude Indicator, Horizontal Situation Indicator, Turn Coordinator, Slip/Skid indicatoriii.ESS BUS 1 – Standby Attitude Indicatoriv.MAIN BUS 1 – Standby Attitude Indicator6.WING FLAPS – see Cirrus Manual (7-22)a.Electrically controlled, single-slotted flapsb.Flap positions:i.0% - 0°ii.50% - 16°iii.100% - 32°c.Flaps controlled through a motorized linear actuator mechanically connected to both flaps by atorque tubed.Flaps are pow ered by 28 VDC through the 10-amp FLAPS circuit breaker on the NONESS BUSe.Flaps up lights are green, Flaps down lights are yellowf.Flap speeds:i.50% - 119 knotsii.100% - 104 knotsNDING GEAR – see Cirrus Manual (7-24)a.Brakes are hydraulically operated, single-disc type brakesb. A temperature sensitive resistor is mounted to each brake assembly which transmit signals viathe Engine Airframe Unit to the Engine Indicating System for brake temperature caution/warningannunciation8.SEATS – see Cirrus Manual (7-27)a.Do not kneel or stand on the seats. The seat bottoms have an integral aluminum honeycomb coredesigned to crush under impact to absorb downward loads (in the event of a crash)b. A crash sensor under the seat contains an accelerometer. This data is linked to the airbags in theshoulder harness. In the event of rapid deceleration (in the event of a crash) the airbags aredeployed9.ENGINE – see Cirrus Manual (7-30)a.Teledyne Continental IO-360-ES, six cylinder, normally aspirated, fuel-injected engine de-rated at200 HP at 2,700 RPMb.Power (Throttle) Lever: mechanically linked by cables to the air throttle body/fuel-metering valveand to the propeller governori.Moving the throttle adjust the percent power of the enginec.Mixture Control Lever is mechanically linked to the mixture control valve in the engine-driven fuelpump. The Mixture Control Lever is labeled RICH-MIXTURE-CUTOFFd.Alternate Air Control is located on the left console near the pilot’s right knee. Pulling the knobopens the alternate air induction door on the engine induction air manifold, bypassing the airfilter and allows warm unfiltered air to enter the engine10.ENGINE LUBRICATION SYSTEMa.Wet-sump, high-pressure oil system for engine lubrication and coolingb.Oil is drawn from an 8 quart capacity sump through an oil suction strainer screen and directed tothe engine-mounted oil coolerc.Oil cooler is equipped with a pressure relief and temperature control valve set to bypass oil if thetemperature is below 170ºF or the pressure drop is greater than 18 PSId.Bypass or cooled oil is then directed through the 1 quart, full-flow oil filter, a pressure relief valve,and then through oil galleries to the engine rotating parts and piston inner domesplete oil system is located in the engine, the oil filler cap can be accessed through a door onthe top left side of the engine cowling11.IGNITION AND STARTER SYSTEMa. 2 engine-driven magnetos and 2 spark plugs in each cylinder provide engine fuel ignitionb.The right magneto fires the lower right and upper left spark plugsc.The left magneto fires the lower left and upper right spark plugsd. A rotary-type key switch, located on the instrument panel, controls ignition and starter positione.In the OFF position, the starter is electrically isolated, the magnetos are grounded and will notoperatef.Normally, the engine is operated on both magnetos (switch in BOTH position) except for magnetochecks and emergency operationsg.The R and L positions are used for individual magneto checks and for single magneto operationwhen requiredh.When the battery master switch is ON, rotating the switch to the spring loaded START positionenergizes the starter and activates both magnetos. The switch automatically returns to the BOTHposition when releasedi.28 VDC for starter operation is supplied through the 2-amp STARTER circuit breaker on NON-ESSENTIAL BUS12.AIR INDUCTION SYSTEMa.Induction air enters the engine compartment through the 2 inlets in the forward cowlingb.Air passes through a dry-foam induction filter, through the throttle butterfly, into the six-tubeengine manifold, and finally through the cylinder intake ports into the combustion chambersc.Should the dry induction filter become clogged, a pilot controlled alternate induction air door canbe opened, allowing engine operation to continue13.ENGINE EXHUASTa. A muff type heat exchanger, located around the right muffler, provides cabin heat14.ENGINE FUEL INJECTIONa.The multi-nozzle, continuous flow fuel injection system supplies fuel for engine operationb.The engine driven fuel pump draws fuel from the selected wing tank and passes it to the mixturecontrol valve integral to the pumpc.The mixture control valve proportions fuel in response to the pilot operated mixture control leverpositiond.Fuel is then routed to the fuel-metering valve on the air-induction system throttle body. The fuel-metering valve adjusts fuel flow in response to the pilot controlled Power Lever positione.From the metering valve, fuel is directed to the fuel manifold valve (spider) and then to theindividual injector nozzles. The system meters fuel flow in proportion to engine RPM, mixturesetting, and throttle anglef.Mixture can be controlled manuallyg.An electric fuel pump provides fuel boost for vapor suppression and for priming15.ENGINE COOLINGa.Engine components discharge heat to the oil and then to the air passing through the oil cooler,and by discharging heat to air flowing past the engineb.Cooling air enters the engine through 2 inlets in the cowling and aluminum baffles direct the airover the engine cylinders and cooling fins where the heat transfer takes placec.Air exits the cowling through 2 vents in the aft portion of the cowling. No cowl flaps are used16.PROPELLERa.Aircraft is equipped with a constant speed propeller with governor and can be configured witheither a 2 blade propeller (76”) or a 3 blade propeller (74”)b.The propeller governor changes propeller pitch to regulate engine and propeller RPM. Thegovernor sense engine speed by means of flyweights and sense throttle setting by a cableconnected to the power control lever (PCL)c.The PCL position sets an engine percent power. Percent power is a function of engine manifoldabsolute pressure and propeller RPMi.% Power = MAP + RPMd.When the PCL is set it moves a throttle control cable and a governor control cable. The governorcontrol cable moves a screw (up/down) in the propeller governor that moves a set of flyweightsinside the governor.e.The flyweights move in when the engine is set to a higher RPM and out when the engine is set toa lower RPM. The flyweight position (in/out) moves a valve that controls oil flow to the propellerhub piston. The only way to close the valve is when the flyweights return to the neutral position.This “neutral position” is set at 2500 RPM during normal cruise flight and 2700 RPM at maxpower.f.When the aircraft is flying, the position of the flyweights ensures constant RPM. For example, ifthe propeller starts moving faster (i.e. in a descent) than the set RPM level (2500, 2700, etc.) thefly weights will move out, therefore bringing oil into the propeller hub and allowing the pitch ofthe blades to increase (which slows the propeller back down to the desired RPM). The positionof the flyweights ensures that oil is constantly being taken in/out of the propeller hub pistontherefore allowing a constant RPM is held.g.Manifold Absolute Pressure is the air pressure going into the intake of the engine. The PCLdirectly controls the MAP through a throttle cableh.According to the percent power equation: % Power = MAP + RPM, once a given RPM is set theonly variable that needs to be set is MAP in order to give a % Power. When the PCL is set, thephysical position of the throttle sets percent power and the throttle control cable automaticallydetermines MAP in order to produce a constant % Power.17.FUEL SYSTEMa.56 gallon usable wet-wing fuel storage systemb.System:i.29.3 gallon capacity (28 gallon usable) vented integral fuel tankii.Fuel collector sump in each wingiii. 3 position selector valve (LEFT, RIGHT, OFF)iv.Electric fuel pumpv.Engine driven fuel pumpc.Fuel is gravity fed to the associated collector sumps where the engine driven fuel pump drawsfuel through a filter and selector valve to pressure feed the engine fuel injection system. Theelectric fuel pump is provided for priming and vapor suppressiond.The Electric fuel pump is controlled by the fuel pump switch in the cockpit. It is linked with the oilsystem and allows HIGH BOOST PRIME when oil pressure is less than 10 PSI. The LOW BOOSTworks regardless of oil pressure and sends a consistent 4-6 PSI boost to the fuel flow for vaporsuppression in a hot fuel condition.e.The fuel pump operates on 28 VDC through the 5-amp FUEL PUMP circuit breaker on MAIN BUS 2ELECTRICAL SYSTEMf.Aircraft is equipped with a 2 alternator, 2 battery 28 volt direct current (VDC) electrical systemdesigned to reduce the risk of electrical system faultsg.Primary power is supplied through a 28 VDC negative ground electrical system. Electrical powerconsists of 2 alternators controlled by a Master Control Unit (MCU) mounted on the left firewall and 2 batteries for starting and electrical power storageh.Alternator 1 (ALT 1) is a belt driven, 85 amp alternator mounted on the right front of the enginei.Alternator 2 (ALT 2) is a gear driven, 75 amp alternator mounted on the accessory drive at therear of the enginej.ALT 1 is regulated to 28 V and ALT 2 is regulated to 28.75 Vk.Battery 1 (BAT 1) is a 24 volt, 11-amp hour battery mounted on the right firewall. BAT 1 is charged from the Main Distribution Bus 1 in the MCU.l.Battery 2 (BAT 2) is composed of two 12 volt, 7-amp hour batteries connected in series to provide 24 volts and 7-amp hours. BAT 2 is located behind the aft cabin bulkhead below theparachute canister. BAT 2 is charged from the circuit breaker panel ESS BUS 1.See Cirrus POH page 7-47 for complete electrical diagram.CIRRUS SR20 SIMPLIFIED ELECTRICAL DIAGRAM18.STALL WARNINGa.As the airplane approaches a stall, the low pressure on the upper surface of the wings movesforward around the leading edge of the wings. As the low pressure area passes over the stallwarning inlet, a slight negative pressure is sensed by the pressure switch. The pressure switchthen provides a signal to cause the warning horn to sound, the red STALL warning CASannunciation to illuminateb.The system operates through 28 VDC supplied through the 2-amp STALL WARNING circuitbreaker on the ESS BUS 219.PITOT STATIC SYSTEMa.The Pitot-Static system provides ram air and static air pressure to operate the:i.Airspeed Indicator (ASI)ii.Altimeter (ALT)iii.Vertical Speed Indicator (VSI)iv.Air Data Computer (ADC)b.The only “true” Pitot/Static instrument is the Airspeed Indicator. It requires both ram air from thepitot tube and static air from the 2 static ports on the fuselagec.The pitot tube and static ports send direct pressure to the Standby Instruments and are displayeddirectly on the gaugesd.The pitot tube and static ports send direct pressure to an Air Data Computer that preciselyinterprets the data and displays it on the PFDe.In the case of static port blockage, an internal Alternate Static source is located to provide staticpressure from inside the cockpit. The Alternate Static switch is located to the right of the pilot’slegf.In case of pitot tube blockage (e.g. from ice), pitot heat is electrically supplied by 28 VDC fromthe NON ESS BUS.20.AVIONICSa.Integrated Avionics Unit – The MFD and PFD receive information from 2 IAUs. They functionas main communication hubs linking all other instruments with the PFD and MFD. Each containsa GPS/WAAS receiver, VHF communication, Navigation/Glideslope receivers, and a flight directorb.Air Data Computer – processes data from the pitot static system and outside air temperaturesensors. These units provide pressure altitude, airspeed, vertical speed and OAT information tothe systemc.Engine and Airframe Sensors – receives and processes signals from engine and airframesensors and communicates that information to the IAUd.AHRS – provides aircraft attitude and heading information to both the PFD and the primary IAU.The AHRS contains advanced sensors including accelerometers and rate sensors and interfacesthe magnetometer to obtain magnetic field information. It also communicates with the Air DataComputer to obtain air data and with both IAUs to obtain GPS informatione.Magnetometer – measures local magnetic field and sends the data to the AHRS system forprocessing to determine aircraft magnetic headingf.Transponder – communicates with the IAU and is controlled via the PFD soft-keys or the GCUcontroller keypad21.EMERGENCY LOCATOR TRANSMITTERa.Located behind the aft cabin bulkhead to the right of aircraft centerlineb.ELT remote switch is labeled ON-OFF-ARMED, it is selected at ARMED for normal operationc.ELT transmits VHF band audio sweeps on 121.5 Mhz and 243.0 Mhz approximately 0.5 secondsapart22.FIRE EXTINGUISHERa.Halon 1211/1301。
西克 OLS20 轨迹导引传感器 操作说明书
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2操作指南 | OLS208024411.1IY1/2023/04/24 | SICK如有更改,恕不另行通知内容内容1关于本文档的 (5)1.1更多信息 (5)1.2符号和文档约定 (5)2安全信息 (6)2.1规定用途 (6)2.2违规使用 (6)2.3关于 UL 认证的提示 (6)2.4责任范围 (6)2.5对专业人员和操作人员的要求 (7)2.6危险提示与作业安全 (7)2.7维修 (7)3产品说明 (8)3.1产品识别 (8)3.2产品特点 (9)4运输和仓储 (10)4.1运输 (10)4.2运输检查 (10)4.3储存环境 (10)5装配 (11)5.1安装准备 (11)5.2安装传感器 (11)6电气安装 (14)6.1安全性 (14)6.2接口的引脚分配 (15)6.3连接工作电压 (16)6.4CAN 接口 (16)7调试 (17)7.1调试步骤概览 (17)7.2首次运行传感器 (17)7.3使用 CANopen 调试的第一步 (17)7.4使用 Modbus RTU 调试的第一步 (20)8操作 (22)8.1通过 CANopen 操作 (22)8.2通过 Modbus RTU 操作 (27)8.3有关操作的一般提示 (30)9维护 (31)9.1清洁 (31)8024411.1IY1/2023/04/24 | SICK操作指南 | OLS203如有更改,恕不另行通知内容9.2维护 (31)9.3维修 (31)10停机 (32)10.1停用 (32)11故障排除 (33)11.1可能的错误指示 (33)12技术数据 (34)12.1光学元件/特性 (34)12.2供电 (34)12.3接口 (34)12.4输出 (34)12.5环境条件 (35)12.6设计结构 (35)13附件 (36)14许可证 (37)15附件 (38)15.1合规性和证书 (38)4操作指南 | OLS208024411.1IY1/2023/04/24 | SICK如有更改,恕不另行通知1关于本文档的1.1更多信息如需查看产品页面的更多信息,请访问 SICK Product ID:/{P/N}/{S/N}。
LX20 LX20R 用户手册说明书
USER MANUAL2020IMPORT ANT SAFETY INSTRUCTIONSWARNING: When using electric products, basic cautions should always be followed, including the following.1. Read all safety and operating instructions before using this product2. The product should be powered by a three pin `grounded (or earthed) plug connected to a power socket with a grounded earth outlet.3. All safety and operating instructions should be retained for future reference4. Obey all cautions in the Operating instructions and on the back of the unit5. All operating instructions should be followed6. This product should not be used near water, i.e. a bathtub, sink, swimming pool, wet basement, etc.7. This product should be located so that its position does not interfere with its proper ventilation. It should not be placed flat against a wall or placed in a built up enclosure that will impede the flow of cooling air.8. This product should not be placed near a source of heat such as stove, radiator, or another heat producing amplifier.9. Connect only to a power supply of the type marker on the unit adjacent to the power supply cord.10.Never break off the ground pin on a power supply cord.11.Power supply cords should always be handled carefully. Never walk or place equipment on power supply cords. Periodically check cords for cuts or signs of stress, especially at the plug and the point where the chord exits the unit.12.The power supply cord should be unplugged when the unit is to be unused for long periods of time.13.If this product is to be mounted in an equipment rack, rear support should be provided.14.The user should allow easy access to any mains plug, mains coupler and mains switch used in conjunction with this unit thus making it readily operable.15.Metal parts can be cleaned with a damp cloth. The vinyl covering used on some units can be cleaned with a damp cloth or ammonia based household cleaner if necessary. Disconnect the unit from the power supply before cleaning.16.Care should be taken so that objects do not fall and liquids are not spilled into the unit through any ventilation holes or openings. On no account place drinks on the unit.17. A qualified service technician should check the unit if:18.The user should not attempt to service the equipment. All service work is done by a qualified service technician.19. Exposure to extremely high noise levels may cause a permanent hearing gloss. Individuals vary considerably in susceptibility to noise induced hearing loss, but nearly everyone will lose some hearing if exposed to sufficiently intense noise for a sufficient time. The U.S. Government's Occupational Safety and Health Administration (OSHA) has specified the following permissible noise level exposure. Duration Per Day In Hours Sound Level dBA, slow response8 9069249539721001 ½1021105½110¼ or less 115According to OSHA, any exposure in excess of the above permissible limits could result in some hearing loss. Ear plugs or protectors in the ear canals or over the ears must beworn when operating this amplification system in order to prevent a permanent hearing loss if exposure exceeds the limits set forth above. T o ensure against potentially dangerous exposure to high sound pressure levels it is recommended that all persons exposed to equipment capable of producing high sound pressure levels such as this amplification system be protected by hearing protectors while this unit is in operation.The power cord has been damagedAnything has fallen or spilled into the unit The unit does not appear to operate correctlyThe unit has been dropped or the enclosure damaged.BEFORE SWITCHING ONAfter unpacking your amplifier check that it is factory fitted with a three pin 'grounded' (or earthed) plug. Before plugging into the power supply ensure you are connecting to a grounded earth outlet.If you should wish to change the factory fitted plug yourself, ensure that the wiring convention applicable to the country where the amplifier is to be used is strictly conformed to. A s an example in the United Kingdom the cable colour code for connections are as follows.NOTEThis manual has been written for easy access of information. The front and rear panels are graphically illustrated, with each control and feature numbered. For a description of the function of each control feature, simply check the number with the explanations adjacent to each panel.Y our Laney amplifier has undergone a thorough two stage, pre-delivery inspection, involving actual play testing.When you first receive your Laney guitar amplifier, follow these simple procedures:(i) Ensure that the amplifier is the correct voltage for the country it is to be used in.ii) Connect your instrument with a high quality shielded instrument cable. Y ou have probably spent con siderable money on your amplifier and guitar - don’t use poor quality cable it won’t do your gear justice.Please retain your original carton and packaging so in the unlikely event that some time in the future your amplifier should require servicing you will be able to return it to your dealer securely packed.Care of your Laney amplifier will prolong it's life.....and yours!EARTH OR GROUND - GREEN/YELLOW NEUTRAL - BLUELIVE - BROWNINTRODUCTIONThe LX20 and LX20R products are open back split channel guitar combos loaded with 8 inch loudspeakers. They have a splitchannel preamp layout, which gives you separate clean and drive level controls through a shared master EQ with bass, mid and treble. They feature headphone sockets for private listening; CD/Line in socket should you need to play along to a CD/MP3 and aheadphone socket for some private time without waking the neighbours. Additionally the LX20R features a built in spring line reverb with master level control.An explanation of these features follows on pages 6-8.Dear Player,Thank you very much for purchasing your new Laney product and becoming part of the worldwide Laney family. Each and every Laney unit is designed and built with the utmost attention to care and detail, so I trust yours will give you many years of ney products have a heritage which stretches back to 1967 when I first began building valve amplifiers in my parent’s garage. Since then we have moved on from strength to strength developing an extensive range of guitar, bass, public address and keyboard amplification products along with a list of Laney endorsees that includes some of the world’s most famous and respected musicians. At the same time we believe we have not lost sight of the reason Laney was founded in the first place - a dedication to building great sounding amplification for working musicians. Warm Regards,Lyndon Laney CEOThis socket should be used for connecting your instrument to the amplifier. Only use a good quality screened cable.Controls the volume level of the clean channel.Switch in to activate the overdrive ‘Crunch’ channel.Indicates that the drive channel is active.Controls the crunch channel gain, low down for classic rock and blues, higher up for hard rock and metal.... the higher you goControls the amount of bass or bottom end present in your sound.Controls the amount of mid present in you sound.Controls the amount of treble present in your sound.ANEL CONTROLSLaneyOPERATING INSTRUCTIONS4Controls the amount of reverb applied to the signal. (LX20R only)Fancy playing along with a backing track? Connect your CD/MP3 player here.Don’t want to wake your neighbours? Connect your headphones here. The internal loudspeaker is automatically switched off.When ‘on’ Indicates that power is connected to the unit and it is ready to go.(Always switch off and disconnect the power cord when not in use)Main power switch for the unit.Power inlet socket. Connect to your power source. Make sure the specified voltage is correct for your country!Displays the model number, power requirements and serial number of the unit.1617SAMPLE SYSTEMBLOCK DIAGRAMQUICK START SETTINGS - Suggestions only, experiment!719310460582V OLUME D RIVE719310460582C RUNCH 719310460582719310460582719310460582I NPUT 77119933101044660558822EVERBCD/L INE I NP HONES1E QUALISATIONLX20RININOUTGeneral NotesAmplifier connection: In order to avoid damage, it is advisable to establish and follow a pattern for turning on and off your equipment. With all system parts connected, turn on source equipment, tape decks, cd players, mixers, effects processors etc.BEFORE turning on your guitar amplifier. Many products have large transient surges at turn on and off which can cause damage to your speakers. By turning on your guitar amplifier LAST and making sure its Volume control is set to minimum any transients from other equipment will not reach your loudspeakers. Wait until all system parts have stabilised; usually a couple of seconds. Similarly when turning off your system always turn down the Volume control on your guitar amplifier and then turn off its power before turning off other equipment.Cables: never use shielded or microphone cable for any speaker connections as this will not be substantial enough to handle the amplifier load and could cause damage to your amplifier system.Caution: These professional loudspeaker systems are capable of generating very high sound pressure levels. Use care withplacement and operation to avoid exposure to excessive levels that can cause permanent hearing damage. (Refer to guidelines on page 2)Servicing: The user should not attempt to service these products. Refer all servicing to qualified service personnel.QUICK ST ART SETTINGS - continued 719310460582V OLUME D RIVE719310460582C RUNCH 719310460582719310460582719310460582I NPUT 77119933101044660558822EVERBCD/L INE I NP HONES1E QUALISATIONLX20RINSPECIFICA TIONS Supply Voltage ~100V , ~120V , ~220V , ~230V , ~240V 50/60Hz Factory Option Mains Fuse Not user changeablePower Consumption 30WOutput Power Rating 15WLoudspeaker 8” Custom Designed DriverFeatures Rugged constructionTEC T ube Emulating T echnologyHeadphone socketCD In (10K Input impedance)(Nominal 300mV Input level)Springline Reverb LX20R onlyEQ Passive Bass, Middle and T rebleInput Impedance 1MOhm/47pFSize 357*360*210(H*W*D)Unit Weight 6.9 KgPacking Weight 8.0 KgThis product conforms to: European EMC directive(2004/108/EC), Low Voltage Directive (72/23/EEC) and CE mark Directive (93/68/EEC)Page 11 /12LaneyOPERATING INSTRUCTIONSIn the interest of continued product development, Laney Reserves the right to amend product specification without prior notification.POWER TO THE MUSIC Laney@。
a2 SIR-20作业指导书 地面天线
GSSI SIR-20 数据采集作业指导书*.rpj 项目信息文件。
*.cmf 天线参数文件。
*.dzt 实际测量文件。
*.mdb 标记数据库文件。
1.建立文件夹。
C:\LAUREL\20070901LAB.2.选择文件夹。
点SIR-20图标打开软件,选择菜单View Customize,directories->source 和output文件存储目录都选择C:\LAUREL\20070901LAB.3.建立工区项目文件。
File New,在Create New Data Collection Project对话框内输入file Name文件名ceshi, 点Next按钮。
4.项目信息。
Review Project Information,Next。
5.选择数据采集方式。
Data Collect Mode对话框选FREE RUN自由测量/时间触发;选POINT MODE点测;选SURVEY WHEEL测量轮,并标定测量轮;点Next按钮。
2.6GHz 1.6GHz900MHz 400MHz 200MHz100MHz Config Type测量对象concrete concrete concrete utility utility geo Config Name天线 2.6GHz 1.6GHz900MHz400MHz200MHz100MHz Transmit Rate发射率100KHz100KHz100KHz100KHz100KHz50KHz Samp/scan采样/测点512512512512512/1024512/1024 Scans/sec测点/秒100-500100-20050-10050-10050-10015-30 Scans/m 扫描/米100-50-20100-50-20100-50-20100-50-20100-50-2010m/mark 米/标记555555按钮Create New Macro系统自动创建新的天线参数文件900MHz.cmf按钮Attach Existing Macro打开已有天线参数文件900MHzP46R20G12.cmf2.6GHz1600MHz900MHz400MHz200MHz100MHz Position(ns)信号位置10010046464646Range(ns)记录长度121220-2540-100100-150100-200-300 Gain增益NumberOfPoints增益点111-2-3-5555Gain value增益值181812IIR H Low Pass平滑降噪33333IIR H High Pass 消除背景0000IIR V Low Pass(MHz)低通2500800400300IIR V High Pass(MHz)高通2251003025FIR Low Pass(MHz)低通50003000FIR High Pass(MHz)高通250400Stacking 叠加100点测9.测量。
14 SIR-20 测量轮标定.
1.
2.(2)环境影响后评价。选择标定距离,如50米,100米。
3.
4.(1)资质等级。评价机构的环评资质分为甲、乙两个等级。环评证书在全国范围内使用,有效期为4年。天线放在起点。
5.
6.(三)安全预评价程序按calibrate按钮,准备标定。
7.
8.2.环境影响评价的概念
9.
10.在评估经济效益不能直接估算的自然资源方面,机会成本法是一种很有用的评价技术。机会成本法特别适。A.国家根据建设项目影响环境的范围,对建设项目的环境影响评价实行分类管理移动天线到终点。
11.
12.3.评估环境影响的价值(最重要的一步):采用环境经济学的环境经济损益分析方法,对量化后的环境功能损害后果进行货币化估价,即对建设项目的环境费用或环境效益进行估价。按FINISH完成标定。参数大概为470
本章中环境影响评价制度,2010年的真题中全部集中在环境影响评价这一节。环境保护的对象,环境影响评价制度,环境影响评价文件的组成、文件的报批等是历年考试的热点。
1.建设项目环境影响评价文件的报批(5)阐述划分评价单元的原则、分析过程等。
SIR产品工程应用指南
产品调试
❖ FPGA上/下行链路读取: 此页面用于读取SIR设备上下行数据读取,需要关注的参数为:
❖ 输入功率:已开启的通道的输入 功率值; ❖ 隔离度:施主天线和重发天线之间的隔离度; ❖ 整机实际输出功率:SIR整机输出的总功率。
SIR配置界面介绍
产品调试
❖ 衰减器校准
此页面用于内部调试用 请勿操作;
输入功率值: 上一行数据表示上行通道输 入功率电平(数值显示范围0~99); 下一行数据表示下行通道输 入功率电平(数值显示范围0~99)。
增益值:
上一行数据表示上行通道设 置增益(数值显示范围0~99);
下一行数据表示下行通道设 置增益(数值显示范围0~99)。
当下行输入功率过低(<90dBm)时,”INPUT”图标闪烁
2、Our destiny offers not only the cup of despair, but the chalice of opportunity. (Richard Nixon, American President )命运给予我们的不是失望之酒,而是机会之杯。二〇二一年六月十七日2021年6月17日星期四
4、All that you do, do with your might; things done by halves are never done right. ----R.H. Stoddard, American poet做一切事都应尽力而为,半途而废永远不行6.17.20216.17.202110:5110:5110:51:1910:51:19
SIR配置界面介绍
产品调试
❖ FPGA上/下行链路设置页面相关名词说明:
❖ 隔离度增益绑定:SIR模块标称最大干扰抵消能力为15dB(增益比隔离度大15dB),当 环境恶化使得隔离度下降超出SIR的最大抵消能力15dB时,此功能可以自动降低增益使 得SIR设备可以适应环境的变化而不自激。
L20H 说明书 -CH
简介在英国非常自豪的设计,工程和制造狮心王(Lionheart)系列带来精品的单端或并联单端的甲类电子管音调提供给独具慧眼的演奏家,正是他们一直在寻找的一种独特的灵敏的具有英国特色电子管音调黑魔法:在这个吉他手对前置放大器失真产生了一种不健康的迷恋的时代,传说中的电子管功率放大器被使劲推的声音几乎成为了历史。
直到现在!20W并联甲类单端输出级安装在L20H渗出经典,温暖的电子管色调。
你驱动得越重,听起来就越好。
加上有足够的增益为现代的音调,它也有凶猛、侵略性的一面,使它适合任何风格的玩家. 完美的用于工作室和实践使用.每一款 狮心王 Lionheart产品都是由经验丰富的吉他手进行广泛的演奏测试,然后才发货给我们的客户。
只有当设备完成到我们完全满意时,它才被分配到自己的独特的建造编号,然后手工敲击在后面安装的铭牌上。
你的L20H应该给你多年的无故障放大,然而,请花时间阅读本手册和熟悉自己的控制,因为它将允许你得到最好的放大器。
我们希望您喜欢使用您的L20H,就像我们喜欢设计和制作它一样。
来自全体LANEY成员的最美好的祝福高输入:“HI”代表高增益。
这种输入是为低输出电平吉他的连接而设计的,使它非常适合单线圈和低增益双线圈型拾音器。
在这个输入中使用高增益拾取可能会使驱动前置放大器太硬,造成“模糊”的声音。
只能使用优质的吉他电缆.低输入:“LO”代表低增益。
这种输入从高输入衰减了大约50%,是为高输出电平吉他设计的。
它对于从高增益双线圈型拾音器获得“紧密”而不是“糊状”的输出非常有用。
也使用这个输入为最干净的全范围的声音与扩展低端响应。
只能使用优质的吉他电缆.清音音量:设置清音通道的响度。
试着把它调高一点,以驱动功率电子管更重以获得真正的复古声音和感觉只有一个高品质的电子管放大器可以提供. 现在用你的吉他音量来控制失真的程度。
(前进一点为失真,后退一点为清音)明亮:当你的吉他在清音通道时为高音频率增加亮度和活力.当你的吉他在驱动通道时增加边缘和挑选重点. 该开关在清音音量/驱动器控制较低设置时影响更大。
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SIRveyor SIR-20 用户手册劳雷公司2005年1月目录第一部分:启动和基本项目的安装 (1)1.1 系统启动 (1)1.2 软件和新项目设置 (1)1.3 创建新项目 (5)1.4 打开已存在的项目文件 (12)1.5 运行当前的项目文件 (14)第二部分:数据采集格式 (15)2.1 单一的二维文件格式 (15)2.2 数据采集——三维文件格式 (17)2.3做超三维分析需补充的数据采集步骤 (22)附录A:SIRveyor 技术规格 (23)附录B:SIRveyor 用于数据采集的电源和配置 (25)附录C:采样道排列形式 (29)附录D:装好的SIR-20配置 (31)附录E:创建和编辑宏命令 (37)附录F:在SIR-20上使用通用雷达 (39)附录G:普通材料的介电值和术语集 (41)术语集 (42)附录H:数据处理和成像 (44)附录I:SIRveyor 命令按钮 (46)第一部分:启动和基本项目的安装SIRveyor SIR 20 是有2 个硬件道(天线),4个记录道的高性能地质雷达(GPR)系统。
SIRveyor被用来记录、处理和显示地下特征的剖面和三维图象(如果有三维格式采集的资料)。
该系统配有标准的GSSI天线,能被用于各种应用领域,来解决复杂的地下探测问题和构造探测问题。
SIRveyor允许我们:●采集:由一个天线采集到4道的数据由两个天线采集到4道的数据二维格式的单一剖面三维格式数据的采集●野外处理数据●复查和显示二维剖面或三维格式的野外数据,1.1 系统启动1、把选择的电源连接到SIRveyor SIR-20设备上(当只有掌上电脑电池时系统不运行)2、接通计算机;开关位于以太网连接器后边计算机右部的后面。
3、一旦计算机接通,并且SIR-20已插入,则系统就运行。
4、过几分钟,显示器灯将闪两下,然后就保持稳定了。
更多的信息请查附录B。
1.2 软件和新项目设置先打开RADAN系统信息屏幕,就可找到软件版本和序列号。
该屏幕将在30秒后消失,或点击鼠标左键跳到下一屏幕。
为了采集数据,特别设置了SIRveyor 的快捷键。
虽然RADAN软件屏幕和SIRveyor 的屏幕好像相同,但两者的配置是不同的,因而数据不能通过RADAN 快捷键采集。
目录、长度和数据库的系统设置这些命令使你能安装系统,以便在新地区收集数据。
如果你希望继续做先前的项目,就跳到1.4部分打开存在的项目文件。
否则,就按以下步骤进行。
第一步是设置数据目录。
对每个工区或每项工作创建新的数据目录,会使管理数据更容易。
应该先指定一个单独的输出目录路径,以便让软件将已处理的数据放到该输出目录。
1、设置文件信息选择视窗>Customize(用户自选)。
2、选择目录表,然后设置源目录和输出目录。
注释:Customize ——用户自选Directories ——目录Appearance ——状态,外观Database ——数据库Linear Units ——长度Source ——源目录Output ——输出目录OK——确定Cancel——取消Apply——应用Help ——帮助3、选择长度列表,然后设置想要的单位。
注释:Customize ——用户自选Directories ——目录Appearance ——状态,外观Database ——数据库Linear Units ——长度Vertical ——垂直Horizontal ——水平OK——确定Cancel——取消Apply——应用Help ——帮助METER ——米CM ——厘米INCH——英寸FOOT——英尺YARD——码4、选择数据库列表,然后点击要选择的临时数据库标记选项。
注释:No Markers Informaion ——无标记的信息Temporary Markers Database——临时标记数据库Permanent Markers Database——永久标记数据库Customize ——用户自选Directories ——目录Appearance ——状态,外观Database ——数据库Linear Units ——长度OK——确定Cancel——取消Apply——应用Help ——帮助5、一旦正确地设置了这些软件参数,就继续到下一节完成新项目的设置。
注释:Step 1 Create New Project ——第一步创建新项目Step 2 Create New Project file ——第二步创建新项目文件3D Project File ——三维项目文件Step 3 Data Collection Mode ——第三步数据采集模式Step 4 Data Collection Parameters ——第四步数据采集参数Step 5 Attach Macro ——第五步附加宏Step 6 Setting Review –System Initialization ——第六步设置复查——系统初始化Step 7 Run ——运行 Save & Stop——保存和停止 Delete & Stop——删除和停止1.3 创建新项目第一步:创建新项目为了开始一个新项目,选择FILE菜单下的New 或点击New Collect。
对一个新的三维项目,必须点击Create 3D File ,请参阅2.2节。
第二步:创建新项目文件1、进入项目文件名。
在合适的输入框内键入唯一的项目文件名,然后点击Save保存。
如果已经存在一个相同文件名的文件,则将提醒你取代老的文件或改变为新文件名。
(注释:位于该窗口底部的Collect Data Files命令框会自动检查,它不能被关闭。
)注释: Create New Data Collection Project——创建新的数据采集项目“1. Type project name”——键入项目名“2. Save”——保存2、在点击Save后,项目信息对话框就会打开,见下图.注释:Project Information ——项目信息“1. Check path”——核对路径“2. Change ,if required”——如果需要,就改变“3. All white fields are optional”——所有空白的方框都是任选的“4. Click OK”——点击OK3、该窗口允许我们检查文件在计算机里被保存的位置(路径).也允许设置测量时间,题目,和任何能在处理或解释期间起帮助作用的注释.这些区域(字段)都是可选择的.4、点击OK, Select Data Collect Mode 对话框就打开了.第三步:数据采集模式数据采集模式对话控制着数据被采集的方式。
●Free Run ——连续采集数据● Point Mode——点测● Survey Wheel ——测量轮● Gosling ——参见附录F注释:测量轮除了为三维成像采集数据外,还必须与构造扫描系统一起来使用。
Free Run:数据是基于设置在文件宏中的每秒扫描时间和次数来采集的。
即使处于稳定状态,只要叉杆开关是压下的,天线就总是不断进行采集。
Point Mode:随着选择叠加,扫描数是被单个收集的。
Survey Wheel:数据是基于测量轮的旋转而采集的,测量轮的旋转是随着你设置的采样率而变化的。
不旋转,就不采集。
Calibrate:为了在不规则界面上得到准确的数据采样,就需对测量轮能够进行校正。
Enable GPS log:将GPS数据(通用雷达数据)录制在笔记本计算机中的一个文件中,该文件是与GPR.dzt文件分开的。
来自GPR数据的扫描数被输出,然后把它并入GPS数据。
Calibrate Survey Wheel:为了把测量轮调节到草地或不平坦地带那样的不同测量界面,要求必须对测量轮做标定。
在理想条件下(平坦、光滑界面、新轮子)的标定数字如下。
若不正确,你的距离计算将是较差的(较远的)。
标定测量轮:1.点击标定按钮.在测量界面上测量一个固定距离,至少10英尺或3米。
注释:Select Positioning System——选择定位系统Calibrate ——标定2.把天线的中心放在0位置(只要在起点和停止点是相同的,天线的任何部分都可以采用)。
(注释:Survey Wheel Calibration——测量轮标定)3.点击开始.测量标定线开始完成4.把天线拉出该距离的长度.5.点击完成.6.点击Save保存.7.一旦标定过程完成,每单位的信号数就出现了.8.重复几次以确信结果..第四步:设置数据采集参数.图注释:Data Collection Parameters ——数据采集参数 Transmit Rate ——发射率数据采集参数(该图用于二维采集。
三维采集的参见2.2节)1——Configuration Type(排列类型):天线选择方式有默认设置,用户设置。
在项目头设置天线名。
2——Configuration Name (排列名称):为多级记录道数据采集选择记录道,同时选择多级天线。
()3——# of Channels:为采集数据所选择的道号。
4——Samples/scan:每次扫描所采集到的样品数,这些选择要预先设置。
5——Scans/second:每秒钟采集到的扫描数,它控制着系统的速度。
6——Dielectric Constant:被测量的介电值控制着深度刻度的精确度。
7——Scans/unit(ft or m):使用测量轮时的数据采样率。
8——Unit/mark:当使用测量轮时,每X英尺/米所自动插入的标号。
9——Antenna Name(天线名):为多道数据采集选择天线。
10——Transmitter(发射器):为每道采集到的数据,指定发射器的位置。
11——Receiver(接收器):为每道采集到的数据,指定接收器的位置。
12——用于发射器/接收器(天线)1的连接器。
13——用于发射器/接收器(天线)2的连接器。
14——对每道采集的数据,道列表中显示出了发射器和接收器的排列形式。
数据采样:特征4到特征8使你能指定数据采集的采样率。
基于测量类型,目标,和测量模式(自由式,点测式或测量轮式),这些特征可以被调节到最适合项目目的。
排列(配置)类型:一张天线频率列表,可用来识别选那一个天线来做测量。
排列(配置)名称(选择天线):在数据采集中天线数目的预先选择。
发射率:固定在100KHz.道的选择(天线名/发射率):可以有1,2或4个数据道,一个或两个天线。
一个天线包括一个T(发射器)和一个R(接收器)。
对每个数据道,你选择一个T 和一个R。
附录C中提供了一些例子。
对使用一个天线的,系统自动默认单道操作。