Local field dynamics in symmetric Q-Ising neural networks

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Vehicle Dynamics汽车动力学Lecture_3_Review of Vehicle Dynamics 1

Vehicle Dynamics汽车动力学Lecture_3_Review of Vehicle Dynamics 1

p or (roll) q or (pitch) r or (yaw)
Fx Fy Fz
Mx My Mz
y
z
Pitch angle: the angle between x-axis and the horizontal plane. Roll angle: the angle between y-axis and the horizontal plane. Yaw angle: the angle between x-axis and the X-axis of an inertial frame
2011-1-18 Zhao You-qun 8
Simplified Vehicle Rigid Body Equations of Motion
Assume
vehicle is symmetric in the xz plane (Ixy = Iyz = 0) p,q,r,v, and w are small, i.e., their products are negligible. u = uo + u’, where u’ is small compared with uo.
∑M ∑M
y
ɺ = I yy q
z
ɺ ɺ = − I xz p + I zz r
A 13 DoF model is derived using Lagrange’s Eqns. in Venhovens [1993]
2011-1-18 Zhao You-qun 9
Longitudinal Vehicle Motion
Zhao You-qun 10
Input Classification
DA hA B Θ Rxf Fzf a Fxf h W b Rxr A Fzr Fxr Rhx Rhz

基于弹性网和直方图相交的非负局部稀疏编码

基于弹性网和直方图相交的非负局部稀疏编码

DOI: 10. 11772 / j. issn. 1001-9081. 2018071483
基于弹性网和直方图相交的非负局部稀疏编码
*பைடு நூலகம்
万 源,张景会 ,陈治平,孟晓静
( 武汉理工大学 理学院,武汉 430070) ( * 通信作者电子邮箱 Jingzhang@ whut. edu. cn)
摘 要: 针对稀疏编码模型在字典基的选择时忽略了群效应,且欧氏距离不能有效度量特征与字典基之间距离 的问题,提出基于弹性网和直方图相交的非负局部稀疏编码方法( EH-NLSC) 。首先,在优化函数中引入弹性网模型, 消除字典基选择数目的限制,能够选择多组相关特征而排除冗余特征,提高了编码的判别性和有效性。然后,在局部 性约束中引入直方图相交,重新定义特征与字典基之间的距离,确保相似的特征可以共享其局部的基。最后采用多 类线性支持向量机进行分类。在 4 个公共数据集上的实验结果表明,与局部线性约束的编码算法( LLC) 和基于非负 弹性网的稀疏编码算法( NENSC) 相比,EH-NLSC 的分类准确率分别平均提升了 10 个百分点和 9 个百分点,充分体现 了其在图像表示和分类中的有效性。
Key words: sparse coding; elastic net model; locality; histogram intersection; image classification
0 引言
图像分类是计算机视觉领域的一个重要研究方向,广泛 应用于生物特征识别、网络图像检索和机器人视觉等领域,其 关键在于如何提取特征对图像有效表示。稀疏编码是图像特 征表示 的 有 效 方 法。考 虑 到 词 袋 ( Bag of Words,BoW) 模 型[1]和空 间 金 字 塔 匹 配 ( Spatial Pyramid Matching,SPM) 模 型[2]容易造成量化误差,Yang 等[3] 结合 SPM 模型提出利用 稀疏编 码 的 空 间 金 字 塔 的 图 像 分 类 算 法 ( Spatial Pyramid Matching using Sparse Coding,ScSPM) ,在图像的不同尺度上 进行稀疏编码,取得了较好的分类效果。在稀疏编码模型中, 由于 1 范数在字典基选择时只考虑稀疏性而忽略了群体效 应,Zou 等[4]提出一种新的正则化方法,将弹性网作为正则项 和变量选择方法。Zhang 等[5]提出判别式弹性网正则化线性

abaqus结构分析单元类型

abaqus结构分析单元类型

;this wordfile adds the code folding function which is useful to ignore rows of numbers,enjoy~;updated in 20130116, based on the wordfile "abaqus_67ef(20080603)";Syntax file for abaqus v6.12 keywords ,code folding enabled;add *ANISOTROPIC *ENRICHMENT *LOW -DISPLACEMENT HYPERELASTIC;newly add /C?"ElementType";delete DISPLACEMENT;delete MASS in /C2"Keywords2"/L29"abaqus_612" Nocase File Extensions = inp des dat msg/Delimiters = ~!@$%^&()_-+=|\/{}[]:;"'<> ,.?//Function String = "%[ ^t]++[ps][a-z]+ [a-z0-9]+ ^(*(*)^)*{$"/Function String 1 = "%[ ^t]++[ps][a-z]+ [a-z0-9]+ ^(*(*)^)[ ^t]++$"/Member String = "^([A-Za-z0-9_:.]+^)[ ^t*&]+$S[ ^t]++[(=);,]"/Variable String = "^([A-Za-z0-9_:.]+^)[ ^t*&]+$S[ ^t]++[(=);,]"/Open Fold Strings = "*" "**""***"/Close Fold Strings = "*" "**""***"/C1"Keywords1" STYLE_KEYWORD*ACOUSTIC *ADAPTIVE *AMPLITUDE *ANISOTROPIC *ANNEAL *AQUA *ASSEMBLY *ASYMMETRIC *AXIAL *BASE *BASELINE *BEAM*BIAXIAL *BLOCKAGE *BOND *BOUNDARY *BRITTLE *BUCKLE *BUCKLING *BULK *C *CAP *CAPACITY *CAST *CAVITY *CECHARGE*CECURRENT *CENTROID *CFILM *CFLOW *CFLUX *CHANGE *CLAY *CLEARANCE *CLOAD *CO *COHESIVE *COMBINED *COMPLEX*CONCRETE *CONDUCTIVITY *CONNECTOR *CONSTRAINT *CONTACT *CONTOUR *CONTROLS *CORRELATION *COUPLED *COUPLING*CRADIATE *CREEP *CRUSHABLE *CYCLED *CYCLIC *D *DAMAGE *DAMPING *DASHPOT *DEBOND *DECHARGE *DECURRENT*DEFORMATION *DENSITY *DEPVAR *DESIGN *DETONATION *DFLOW *DFLUX *DIAGNOSTICS *DIELECTRIC *DIFFUSIVITY*DIRECT *DISPLAY *DISTRIBUTING *DISTRIBUTION *DLOAD *DRAG *DRUCKER *DSA *DSECHARGE *DSECURRENT *DSFLOW*DSFLUX *DSLOAD *DYNAMIC *EL *ELASTIC *ELCOPY *ELECTRICAL *ELEMENT *ELGEN *ELSET *EMBEDDED *EMISSIVITY*END *ENERGY *ENRICHMENT *EOS *EPJOINT *EQUATION *EULERIAN *EXPANSION *EXTREME *FABRIC *FAIL *FAILURE*FASTENER *FIELD *FILE *FILM *FILTER *FIXED *FLOW *FLUID *FOUNDATION *FRACTURE *FRAME *FREQUENCY *FRICTION*GAP *GASKET *GEL *GEOSTATIC *GLOBAL *HEADING *HEAT *HEATCAP *HOURGLASS *HYPERELASTIC *HYPERFOAM *HYPOELASTIC*HYSTERESIS *IMPEDANCE *IMPERFECTION *IMPORT *INCIDENT *INCLUDE *INCREMENTATION *INELASTIC *INERTIA*INITIAL *INSTANCE *INTEGRATED *INTERACTION *INTERFACE *ITS *JOINT *JOINTED *JOULE *KAPPA *KINEMATIC*LATENT *LOAD *LOADING *LOW *M1 *M2 *MAP *MASS *MATERIAL *MATRIX*MEMBRANE *MODAL *MODEL *MOHR *MOISTURE*MOLECULAR *MONITOR *MOTION *MPC *MULLINS *NCOPY *NFILL *NGEN *NMAP *NO *NODAL *NODE *NONSTRUCTURAL*NORMAL *NSET *ORIENTATION *ORNL *OUTPUT *PARAMETER *PART *PERIODIC *PERMEABILITY *PHYSICAL *PIEZOELECTRIC*PIPE *PLANAR *PLASTIC *POROUS *POST *POTENTIAL *PRE *PREPRINT *PRESSURE *PRESTRESS *PRINT *PSD *RADIATE*RADIATION *RANDOM *RATE *RATIOS *REBAR *REFLECTION *RELEASE *RESPONSE *RESTART *RETAINED *RIGID *ROTARY*SECTION *SELECT *SFILM *SFLOW *SHEAR *SHELL *SIMPEDANCE *SIMPLE *SLIDE *SLOAD *SOILS *SOLID *SOLUBILITY*SOLUTION *SOLVER *SORPTION *SPECIFIC *SPECTRUM *SPRING *SRADIATE *STATIC *STEADY *STEP *SUBMODEL*SUBSTRUCTURE *SURFACE *SWELLING *SYMMETRIC *SYSTEM *TEMPERATURE *TENSILE *TENSION *THERMAL *TIE *TIME*TORQUE *TRACER *TRANSFORM *TRANSPORT *TRANSVERSE *TRIAXIAL *TRS *UEL *UNDEX *UNIAXIAL *UNLOADING *USER*VARIABLE *VIEWFACTOR *VISCO *VISCOELASTIC *VISCOUS *VOID *VOLUMETRIC *WAVE *WIND-AXISYMMETRIC -DEFINITION -DISPLACEMENT -SIMULATION -SOIL -TENSION /C2"Keywords2"ACTIVATION ADDED AREA ASSEMBLE ASSEMBLY ASSIGNMENT AXIAL BEHAVIOR BODY BULKCASE CAVITY CENTER CHAIN CHANGE CHARGE CLEARANCE COMPACTION COMPONENT COMPRESSION CONDITIONS CONDUCTANCE CONDUCTIVITY CONSTANTS CONSTITUTIVE CONSTRAINT CONTACT CONTROL CONTROLS COPY CORRECTION COULOMB COUPLINGCRACKING CREEP CRITERIA CRITERION CYCLICDAMAGE DAMAGED DAMPING DATA DEFINED DEFINITION DELETE DENSITY DEPENDENCE DEPENDENT DERIVED DETECTIONDIFFUSION DIRECTORY DOFS DYNAMIC DYNAMICSEFFECT EIGENMODES ELASTIC ELASTICITY ELECTRICAL ELEMENT ELSET ENVELOPE EVOLUTION EXCHANGE EXCLUSIONSEXPANSIONFACTORS FAILURE FIELD FILE FLAW FLOW FLUID FLUX FOAM FORMAT FORMULATION FRACTION FREQUENCY FRICTIONGENERAL GENERATE GENERATION GRADIENTHARDENING HEAT HOLD HYPERELASTICINCLUSIONS INERTIA INFLATOR INITIATION INPUT INSTANCE INTEGRAL INTERACTION INTERFERENCE IRONLAYER LEAKOFF LENGTH LINE LINK LOAD LOCKM1 M2 MATERIAL MATRIX MEDIUM MESH METAL MIXTURE MODEL MODES MODULI MODULUS MOTIONNODAL NODE NSET NUCLEATIONORIGIN OUTPUTPAIR PARAMETER PART PARTICLE PATH PENETRATION PLASTIC PLASTICITY POINT POINTS POTENTIAL PRAGER PRINTPROPERTYRADIATION RATE RATIOS REDUCTION REFERENCE REFLECTION REGION RELIEF RESPONSE RESULTS RETENTIONSECTION SCALING SHAPE SHEAR SOLID SOLUTION SPECTRUM STABILIZATION STATE STEP STIFFENING STIFFNESS STOPSTRAIN STRESS SURFACE SWELLING SYMMETRYTABLE TECHNIQUE TEMPERATURE TENSION TEST THERMAL THICKNESS TO TORQUE TRANSFER TRANSPORTVALUE VARIABLES VARIATION VELOCITY VIEWFACTOR VISCOSITYWAVE WEIGHT/C3"ElementType" STYLE_ELEMENTAC1D2 AC1D3 AC2D3 AC2D4 AC2D4R AC2D6 AC2D8 AC3D4 AC3D6 AC3D8 AC3D8R AC3D10 AC3D15 AC3D20 ACAX3 ACAX4ACAX4R ACAX6 ACAX8 ACIN2D2 ACIN2D3 ACIN3D3 ACIN3D4 ACIN3D6 ACIN3D8 ACINAX2 ACINAX3 ASI1 ASI2 ASI2AASI2D2 ASI2D3 ASI3 ASI3A ASI3D3 ASI3D4 ASI3D6 ASI3D8 ASI4 ASI8 ASIAX2 ASIAX3B21 B21H B22 B22H B23 B23H B31 B31H B31OS B31OSH B32 B32H B32OS B32OSH B33 B33HC3D4 C3D4E C3D4H C3D4P C3D4T C3D6 C3D6E C3D6H C3D6P C3D6T C3D8 C3D8E C3D8H C3D8HT C3D8I C3D8IH C3D8PC3D8PH C3D8PHT C3D8PT C3D8R C3D8RH C3D8RHT C3D8RP C3D8RPH C3D8RPHT C3D8RPT C3D8RT C3D8T C3D10 C3D10EC3D10H C3D10I C3D10M C3D10MH C3D10MHT C3D10MP C3D10MPH C3D10MPT C3D10MT C3D15 C3D15E C3D15H C3D15VC3D15VH C3D20 C3D20E C3D20H C3D20HT C3D20P C3D20PH C3D20R C3D20RE C3D20RH C3D20RHT C3D20RP C3D20RPHC3D20RT C3D20T C3D27 C3D27H C3D27R C3D27RH CAX3 CAX3E CAX3H CAX3T CAX4 CAX4E CAX4H CAX4HT CAX4ICAX4IH CAX4P CAX4PH CAX4PT CAX4R CAX4RH CAX4RHT CAX4RP CAX4RPH CAX4RPHT CAX4RPT CAX4RT CAX4T CAX6CAX6E CAX6H CAX6M CAX6MH CAX6MHT CAX6MP CAX6MPH CAX6MT CAX8 CAX8E CAX8H CAX8HT CAX8P CAX8PH CAX8RCAX8RE CAX8RH CAX8RHT CAX8RP CAX8RPH CAX8RT CAX8T CAXA4HN CAXA4N CAXA4RHN CAXA4RN CAXA8HN CAXA8NCAXA8PN CAXA8RHN CAXA8RN CAXA8RPN CCL12 CCL12H CCL18 CCL18H CCL24 CCL24H CCL24R CCL24RH CCL9 CCL9HCGAX3 CGAX3H CGAX3HT CGAX3T CGAX4 CGAX4H CGAX4HT CGAX4R CGAX4RH CGAX4RHT CGAX4RT CGAX4T CGAX6 CGAX6HCGAX6M CGAX6MH CGAX6MHT CGAX6MT CGAX8 CGAX8H CGAX8HT CGAX8R CGAX8RH CGAX8RHT CGAX8RT CGAX8T CIN3D12RCIN3D18R CIN3D8 CINAX4 CINAX5R CINPE4 CINPE5R CINPS4 CINPS5R COH2D4 COH2D4P COH3D6 COH3D6P COH3D8COH3D8P COHAX4 COHAX4P CONN2D2 CONN3D2 CPE3 CPE3E CPE3H CPE3T CPE4 CPE4E CPE4H CPE4HT CPE4I CPE4IHCPE4P CPE4PH CPE4R CPE4RH CPE4RHT CPE4RP CPE4RPH CPE4RT CPE4T CPE6 CPE6E CPE6H CPE6M CPE6MH CPE6MHTCPE6MP CPE6MPH CPE6MT CPE8 CPE8E CPE8H CPE8HT CPE8P CPE8PH CPE8R CPE8RE CPE8RH CPE8RHT CPE8RPCPE8RPH CPE8RT CPE8T CPEG3 CPEG3H CPEG3HT CPEG3T CPEG4 CPEG4H CPEG4HT CPEG4I CPEG4IH CPEG4R CPEG4RHCPEG4RHT CPEG4RT CPEG4T CPEG6 CPEG6H CPEG6M CPEG6MH CPEG6MHT CPEG6MT CPEG8 CPEG8H CPEG8HT CPEG8RCPEG8RH CPEG8RHT CPEG8T CPS3 CPS3E CPS3T CPS4 CPS4E CPS4I CPS4R CPS4RT CPS4T CPS6 CPS6E CPS6M CPS6MTCPS8 CPS8E CPS8R CPS8RE CPS8RT CPS8TDASHPOT1 DASHPOT2 DASHPOTA DC1D2 DC1D2E DC1D3 DC1D3E DC2D3 DC2D3E DC2D4 DC2D4E DC2D6 DC2D6E DC2D8DC2D8E DC3D10 DC3D10E DC3D15 DC3D15E DC3D20 DC3D20E DC3D4 DC3D4E DC3D6 DC3D6E DC3D8 DC3D8E DCAX3DCAX3E DCAX4 DCAX4E DCAX6 DCAX6E DCAX8 DCAX8E DCC1D2 DCC1D2D DCC2D4 DCC2D4D DCC3D8 DCC3D8D DCCAX2DCCAX2D DCCAX4 DCCAX4D DCOUP2D DCOUP3D DGAP DRAG2D DRAG3D DS3 DS4 DS6 DS8 DSAX1 DSAX2EC3D8R EC3D8RT ELBOW31 ELBOW31B ELBOW31C ELBOW32 EMC2D3 EMC2D4 EMC3D4 EMC3D8F2D2 F3D3 F3D4 FAX2 FLINK FRAME2D FRAME3D FC3D4 FC3D6 FC3D8 GAPCYL GAPSPHER GAPUNI GAPUNIT GK2D2 GK2D2N GK3D12M GK3D12MN GK3D18 GK3D18N GK3D2 GK3D2N GK3D4LGK3D4LN GK3D6 GK3D6L GK3D6LN GK3D6N GK3D8 GK3D8N GKAX2 GKAX2N GKAX4 GKAX4N GKAX6 GKAX6N GKPE4 GKPE6GKPS4 GKPS4N GKPS6 GKPS6NHEATCAPIRS21A IRS22A ISL21A ISL22A ITSCYL ITSUNI ITT21 ITT31JOINT2D JOINT3D JOINTCLS3S LS6MASS M3D3 M3D4 M3D4R M3D6 M3D8 M3D8R M3D9 M3D9R MAX1 MAX2 MCL6 MCL9 MGAX1 MGAX2PC3D PIPE21 PIPE21H PIPE22 PIPE22H PIPE31 PIPE31H PIPE32 PIPE32H PSI24 PSI26 PSI34 PSI36Q3D4 Q3D6 Q3D8 Q3D8H Q3D8R Q3D8RH Q3D10M Q3D10MH Q3D20 Q3D20H Q3D20R Q3D20RHR2D2 R3D3 R3D4 RAX2 RB2D2 RB3D2 ROTARYIS3 S3T S3R S3RS S3RT S4 S4T S4R S4RT S4R5 S4RS S4RSW S8R S8R5 S8RT S9R5 SAX1 SAX2 SAX2T SAXA1NSAXA2N SC6R SC6RT SC8R SC8RT SFM3D3 SFM3D4 SFM3D4R SFM3D6 SFM3D8 SFM3D8R SFMAX1 SFMAX2 SFMCL6 SFMCL9SFMGAX1 SFMGAX2 SPRING1 SPRING2 SPRINGA STRI3 STRI65T2D2 T2D2E T2D2H T2D2T T2D3 T2D3E T2D3H T2D3T T3D2 T3D2E T3D2H T3D2T T3D3 T3D3E T3D3H T3D3TWARP2D3 WARP2D4。

Localization Phenomena in Mistimed Assemblies with Cyclic Symmetry Part I

Localization Phenomena in Mistimed Assemblies with Cyclic Symmetry Part I

1Hale Waihona Puke Paper received at ASME Headquarters, September 22, 1987.
the modal properties of tuned and mistuned systems and showed that the multiple eigenvalues of the tuned system are split by the introduction of blade mistuning, thereby resulting in the apparition of several additional peaks in the frequency response. Besides these general findings, though, there is quantitative and even qualitative disagreement among these studies. For instance, the increase in maximum amplitude due to mistuning was found to be different by various researchers (Whitehead, 1966, El-Bayoumy and Srinivasan, 1975, Dye and Henry, 1969, Ewins, 1969, 1973, 1976a, 1976b, Srinivasan and Frye, 1976, Fabunmi, 1980, Sogliero and Srinivasan, 1980, Griffin and Hoosac, 1984, Afolabi, 1985a, Basu and Griffin, 1985). Also, the blade with the largest amplitude was qualitatively inconsistent comparing the findings of various studies. Afolabi (1985a) concluded that the blade with the largest amplitude is likely to be the blade with the most mistuning, while El-Bayoumy and Srinivasan (1975) and Griffin and Hoosac (1984) did not reach this conclusion. Finally, the effect of the mistuning standard deviation on the rotor's largest amplitude was investigated by Sogliero and Srinivasan (1980) and Griffin and Hoosac (1984), and, again, conflicting conclusions were reached. These discrepancies may originate from the different models and parameter values used in the studies. The authors believe that the widely different values and models used for the structural coupling may be one of the primary causes for the large variations that have been observed in mistuning sensitivity. Note that, even though the effects of structural coupling on sensitivity to mistuning have been studied by various authors (Kielb and Kaza, 1984, Srinivasan and Frye, 1976, Basu and Griffin, 1985), structural

PPT-国家自然科学基金委创新群体报告.

PPT-国家自然科学基金委创新群体报告.
Low Energy Dynamics of QCD & Realistic AdS/QCD
Yue-Liang Wu
Kavli Institute for Theoretical Physics China
Key Laboratory of Frontiers in Theoretical Physics Institute of Theoretical Physics, Chinese Acadeny of Sciences 2010.11.25
Loop Regularization
Simple Prescription: in ILIs, make the following replacement
With the conditions
So that
Gauge Invariant Consistency Conditions
Checking Consistency Condition

Indication: existence in any case a characterizing energy scale (CES) M_c At sufficiently low energy then means: E << M_c QFTs

Why Quantum Field Theory So Successful
Any quantum theory that at sufficiently low energy and large distances looks Lorentz invariant and satisfies the cluster decomposition principle will also at sufficiently low energy look like a quantum field theory.

INSEARCHOFEXCELLENCE

INSEARCHOFEXCELLENCE

IN SEARCH OF EXCELLENCEExcellence is a journey and not a destination. In science itimplies perpetual efforts to advance the frontiers of knowledge.This often leads to progressively increasing specialization andemergence of newer disciplines. A brief summary of salientcontributions of Indian scientists in various disciplines isintroduced in this section.92P U R S U I T A N D P R O M O T I O N O F S C I E N C EThe modern period of mathematics research in India started with Srinivasa Ramanujan whose work on analytic number theory and modular forms ishighly relevant even today. In the pre-Independence period mathematicians like S.S. Pillai,Vaidyanathaswamy, Ananda Rau and others contributed a lot.Particular mention should be made of universities in Allahabad, Varanasi, Kolkata,Chennai and Waltair and later at Chandigarh,Hyderabad, Bangalore and Delhi (JNU). The Department of Atomic Energy came in a big way to boost mathematical research by starting and nurturing the Tata Institute of Fundamental Research (TIFR), which, under the leadership of Chandrasekharan, blossomed into a great school of learning of international standard. The Indian Statistical Institute, started by P.C. Mahalanobis,made its mark in an international scene and continues to flourish. Applied mathematics community owes a great deal to the services of three giants Ñ N.R. Sen, B.R. Seth and P .L. Khastgir. Some of the areas in which significant contributions have been made are briefly described here.A LGEBRAOne might say that the work on modern algebra in India started with the beautiful piece of work in 1958 on the proof of SerreÕs conjecture for n =2. A particular case of the conjecture is to imply that a unimodular vector with polynomial entries in n vari-ables can be completed to a matrix of determinantone. Another important school from India was start-ed in Panjab University whose work centres around Zassanhaus conjecture on groupings.A LGEBRAIC G EOMETRYThe study of algebraic geometry began with a seminal paper in 1964 on vector bundles. With further study on vector bundles that led to the mod-uli of parabolic bundles, principle bundles, algebraic differential equations (and more recently the rela-tionship with string theory and physics), TIFR has become a leading school in algebraic geometry. Of the later generation, two pieces of work need special mention: the work on characterization of affine plane purely topologically as a smooth affine surface, sim-ply connected at infinity and the work on Kodaira vanishing. There is also some work giving purely algebraic geometry description of the topologically invariants of algebraic varieties. In particular this can be used to study the Galois Module Structure of these invariants.L IE T HEORYThe inspiration of a work in Lie theory in India came from the monumental work on infinite dimensional representation theory by Harish Chandra, who has, in some sense, brought the sub-ject from the periphery of mathematics to centre stage. In India, the initial study was on the discrete subgroups of Lie groups from number theoretic angle. The subject received an impetus after an inter-national conference in 1960 in TIFR, where the lead-ing lights on the subject, including A. Selberg partic-M ATHEMATICAL S CIENCESC H A P T E R V I Iipated. Then work on rigidity questions was initiat-ed. The question is whether the lattices in arithmetic groups can have interesting deformations except for the well-known classical cases. Many important cases in this question were settled.D IFFERENTIALE QUATIONA fter the study of L-functions were found to beuseful in number theory and arithmetic geome-try, it became natural to study the L-functions arising out of the eigenvalues of discrete spectrum of the dif-ferential equations. MinakshisundaramÕs result on the corresponding result for the differential equation leading to the Epstein Zeta function and his paper with A. Pleijel on the same for the connected com-pact Riemanian manifold are works of great impor-tance. The idea of the paper (namely using the heat equation) lead to further improvement in the hands of Patodi. The results on regularity of weak solution is an important piece of work. In the later 1970s a good school on non-linear partial differential equa-tions that was set up as a joint venture between TIFR and IISc, has come up very well and an impressive lists of results to its credit.For differential equations in applied mathematics, the result of P.L. Bhatnagar, BGK model (by Bhatnagar, Gross, Krook) in collision process in gas and an explanation of Ramdas Paradox (that the temperature minimum happens about 30 cm above the surface) will stand out as good mathematical models. Further significant contributions have been made to the area of group theoretic methods for the exact solutions of non-liner partial differential equations of physical and engineering systems.E RGODIC T HEORYE arliest important contribution to the Ergodic the-ory in India came from the Indian Statistical Institute. Around 1970, there was work on spectra of unitary operators associated to non-singular trans-formation of flows and their twisted version, involv-ing a cocycle.Two results in the subjects from 1980s and 1990s are quoted. If G is lattice in SL(2,R) and {uÐt} a unipotent one parameter subgroup of G, then all non-periodic orbits of {uÐt} on GÐ1 are uniformly distributed. If Q is non-generate in definite quadratic form in n=variables, which is not a multiple of rational form, then the number of lattice points xÐwith a< ½Q(x)½< b, ½½x½½< r, is at least comparable to the volume of the corresponding region.N UMBER T HEORYT he tradition on number theory started with Ramanujan. His work on the cusp form for the full modular group was a breakthrough in the study of modular form. His conjectures on the coefficient of this cusp form (called RamanujanÕs tau function) and the connection of these conjectures with conjectures of A. Weil in algebraic geometry opened new research areas in mathematics. RamanujanÕs work (with Hardy) on an asymptotic formula for the parti-tion of n, led a new approach (in the hands of Hardy-Littlewood) to attack such problems called circle method. This idea was further refined and S.S. Pillai settled WaringÕs Conjecture for the 6th power by this method. Later the only remaining case namely 4th powers was settled in mid-1980s. After Independence, the major work in number theory was in analytic number theory, by the school in TIFR and in geometry of numbers by the school in Panjab University. The work on elliptic units and the con-struction of ray class fields over imaginary quadratic fields of elliptic units are some of the important achievements of Indian number theory school. Pioneering work in BakerÕs Theory of linear forms in logarithms and work on geometry of numbers and in particular the MinkowskiÕs theorem for n = 5 are worth mentioning.P ROBABILITY T HEORYS ome of the landmarks in research in probability theory at the Indian Statistical Institute are the following:93 P U R S U I T A N D P R O M O T I O N O F S C I E N C Eq A comprehensive study of the topology of weak convergence in the space of probability measures on topological spaces, particularly, metric spaces. This includes central limit theorems in locally compact abelian groups and Milhert spaces, arithmetic of probability distributions under convolution in topological groups, Levy-khichini representations for characteristic functions of probability distributions on group and vector spaces.q Characterization problems of mathematical statistics with emphasis on the derivation of probability laws under natural constraints on statistics evaluated from independent observations.q Development of quantum stochastic calculus based on a quantum version of ItoÕs formula for non-commutative stochastic processes in Fock spaces. This includes the study of quantum stochastic integrals and differential equations leading to the construction of operator Markov processes describing the evolution of irreversible quantum processes.q Martingale methods in the study of diffusion processes in infinite dimensional spaces.q Stochastic processes in financial mathematics.C OMBINATORICST hough the work in combinatorics had been ini-tiated in India purely through the efforts of R.C.Bose at the Indian Statistical Institute in late thirties, it reached its peak in late fifties at the University of North Carolina, USA, where he was joined by his former student S.S.Shrikhande. They provided the first counter-example to the celebrat-ed conjecture of Euler (1782) and jointly with Parker further improved it. The last result is regarded a classic.In the absence of these giants there was practically no research activity in this area in India. However, with the return of Shrikhande to India in 1960 activities in the area flourished and many notable results in the areas of embedding of residual designs in symmetric designs, A-design conjecture and t-designs and codes were reported.T HEORY OF R ELATIVITYI n a strict sense the subject falls well within the purview of physics but due to the overwhelming response by workers with strong foundation in applied mathematics the activity could blossom in some of the departments of mathematics of certain universities/institutes. Groups in BHU, Gujarat University, Ahmedabad, Calcutta University, and IIT, Kharagpur, have contributed generously to the area of exact solutions of Einstein equations of gen-eral relativity, unified field theory and others. However, one exact solution which has come to be known as Vaidya metric and seems to have wide application in high-energy astrophysics deserves a special mention.N UMERICAL A NALYSIST he work in this area commenced with an attempt to solve non-linear partial differential equations governing many a physical and engineering system with special reference to the study of Navier-Stabes equations and cross-viscous forces in non-Newtonian fluids. The work on N-S equation has turned out to be a basic paper in the sense that it reappeared in the volume, Selected Papers on Numerical Solution of Equations of Fluid Dynamics, Applied Mathematics, through the Physical Society of Japan. The work on non-Newtonian fluid has found a place in the most prestigious volume on Principles of Classical Mechanics & Field Theory by Truesdell and Toupin. The other works which deserve mention are the development of extremal point collocation method and stiffy stable method.A PPLIED M ATHEMATICST ill 1950, except for a group of research enthusi-asts working under the guidance of N.R.Sen at Calcutta University there was practically no output in applied mathematics. However, with directives from the centre to emphasize on research in basic94P U R S U I T A N D P R O M O T I O N O F S C I E N C Eand applied sciences and liberal central fundings through central and state sponsored laboratories, the activity did receive an impetus. The department of mathematics at IIT, Kharagpur, established at the very inception of the institute of national importance in 1951, under the dynamic leadership of B.R.Seth took the lead role in developing a group of excellence in certain areas of mathematical sciences. In fact, the research carried out there in various disciplines of applied mathematics such as elasticity-plasticity, non-linear mechanics, rheological fluid mechanics, hydroelasticity, thermoelasticity, numerical analysis, theory of relativity, cosmology, magneto hydrody-namics and high-temperature gasdynamics turned out to be a trend setting one for other IITs, RECs, other Technical Institutes and Universities that were in the formative stages. B.R. SethÕs own researches on the study of Saint-VenamtÕs problem and transi-tion theory to unify elastic-plastic behaviour of mate-rials earned him the prestigious EulerÕs bronze medal of the Soviet Academy of Sciences in 1957. The other areas in which applied mathematicians con-tributed generously are biomechanics, CFD, chaotic dynamics, theory of turbulence, bifurcation analysis, porous media, magnetics fluids and mathematicalphysiology.95 P U R S U I T A N D P R O M O T I O N O F S C I E N C E。

具有反射群对称性的球面图案自动生成

具有反射群对称性的球面图案自动生成

具有反射群对称性的球面图案自动生成王新长;刘满凤;欧阳培昌【摘要】Equivariant mapping method is not only difficult to be implemented, but also constrained by the order of symmetry group. Drawn on the experience of the invariant theory of finite reflection group, this paper proposes an invariant mapping method to yield aesthetical spherical patterns and establishes a method to create infinite spherical patterns automatically. This method not only is easy to be implemented, but also can be extended to deal with the cases in the higher dimensional spaces.%等变映射方法在生成艺术图案中具有构造困难,受对称群阶数瓶颈限制等缺点。

借鉴有限反射群不变论的结论,提出不变映射方法生成具有正多面体反射群对称性的球面艺术图案,建立了一种可生成无穷无尽球面图案的自动化方法。

该方法不仅实施容易,且可类似地推广到高维空间中。

【期刊名称】《计算机工程与应用》【年(卷),期】2013(000)023【总页数】4页(P27-30)【关键词】有限反射群;正多面体;不变论;不变映射【作者】王新长;刘满凤;欧阳培昌【作者单位】江西财经大学信息管理学院,南昌 330013; 井冈山大学数理学院,江西吉安 343009;江西财经大学信息管理学院,南昌 330013;井冈山大学数理学院,江西吉安 343009【正文语种】中文【中图分类】TP391利用计算机技术自动生成艺术图案是一个实用的新兴课题,借助迅猛发展精工技艺(如激光喷墨、3D打印等),其研究结果可以广泛地应用到壁纸、瓷砖、包装材料、纺织等与装饰领域有关的行业,生成美观的工艺品,不仅可以满足人们对于美的追求与赏析,而且具有可观的经济价值。

Structural Analyses

Structural Analyses

1. Structural AnalysesStructural analysis is probably the most common application of the finite element method as it implies bridges and buildings, naval, aeronautical, and mechanical structures such as ship hulls, aircraft bodies, and machine housings, as well as mechanical components such as pistons, machine parts, and tools.Steps to solving the present problem by ANSYS:Like solving any problem analytically, we need to define (1) solution domain, (2) the physical model, (3) boundary conditions and (4) the physical properties. We then solve the problem and present the results. In numerical methods, the main difference is an extra step called mesh generation. This is the step that divides the complex model into small elements that become solvable in an otherwise too complex situation. Below describes the processes in terminology slightly more attune to the software.Construct a two or three dimensional representation of the object to be modeled and tested using the work plane coordinate system within ANSYS.Now that the part exists, define a library of the necessary materials that compose the object (or project) being modeled. This includes thermal and mechanical properties.At this point ANSYS understands the makeup of the part. Now define how the modeled system should be broken down into finite pieces.Once the system is fully designed, the last task is to burden the system with constraints, such as physical loadings or boundary conditions.This is actually a step, because ANSYS needs to understand within what state (steady state, transient… etc.) the problem must be solved.After the solution has been obtained, there are many ways to present A NSYS’ results, choose from many options such as tables, graphs, and contour plots.Static Analysis - Used to determine displacements, stresses, etc. under static loading conditions. ANSYS can compute both linear and nonlinear static analyses. Nonlinearities can include plasticity, stress stiffening, large deflection, large strain, hyper elasticity, contact surfaces, and creep.Transient Dynamic Analysis - Used to determine the response of a structure to arbitrarily time-varying loads. All nonlinearities mentioned under Static Analysis above are allowed.Buckling Analysis - Used to calculate the buckling loads and determine the buckling mode shape. Both linear (eigenvalue) buckling and nonlinear buckling analyses are possible.In addition to the above analysis types, several special-purpose features are available such as Fracture mechanics, Composite material analysis, Fatigue, and both p-Method and Beam analyses.A modal analysis is typically used to determine the vibration characteristics (natural frequencies and mode shapes) of a structure or a machine component while it is being designed. It can also serve as a starting point for another, more detailed, dynamic analysis, such as a harmonic response or full transient dynamic analysis.Modal analyses, while being one of the most basic dynamic analysis types available in ANSYS, can also be more computationally time consuming than a typical static analysis. A reduced solver, utilizing automatically or manually selected master degrees of freedom is used to drastically reduce the problem size and solution time. Multiple time saving modal solution methods are available in ANSYS for mode extraction from the reduced solution, such as:Block Lanczos method – typically used for large symmetric eigenvalue problems, this method utilizes a sparse matrix solverPCG Lanczos method - used for very large symmetric eigenvalue problems (500,000+ DOFs), and is especially useful to obtain a solution for the lowest modes to learn how the model will behave.Subspace method - used for large symmetric eigenvalue problems, though in most cases the Block Lanczos method is preferred for shorter run times with equivalent accuracyReduced (Householder) method - faster than the subspace method because it uses reduced (condensed) system matrices to calculate the solution, but is normally less accurate because the reduced mass matrix is approximateUnsymmetric method - used for problems with unsymmetric matrices, such as fluid-structure interaction problemsDamped method - used for problems where damping cannot be ignored, such as journal bearing problems.QR damped method - faster than the damped method, this method uses the reduced modal damped matrix to calculate complex damped frequencies.Finite element representation of B ody in White model of prototype SUV as simulated with Block Lanczos method modal analysis to find critical low frequency natural vibration modes which can cause passenger discomfort if excited.l.3 Transient Dynamic AnalysisTransient dynamic analysis (sometimes called time-history analysis) is a technique used to determine the dynamic response of a structure under the action of any generaltime-dependent loads. Transient Dynamics analyses are use to determine the time-varying displacements, strains, stresses, and forces in a structure as it responds to any combination of static and time varying loads while simultaneously considering the effects of inertia or damping.Transient dynamic analysis in ANSYS can be broadly classified as one of two types:1. Rigid Dynamics – In an assembly, all parts are considered to be infinitely stiff, no mesh is required, and a special solver is used to drastically reduce the amount computational resources required. The primary focus of a rigid dynamics simulation is mechanism operation, part velocities and accelerations, and joint forces encountered during the range of mechanism motion. The new ANSYS Rigid Dynamics product is used for this type of simulationCombined Rigid and Flexible Dynamics simulation done on suspension assembly to investigate upper and lowerpotential A-arm failure mechanisms2. Flexible Dynamics – Some or all parts of an assembly are meshed and considered flexible based on the material that they are made from. Typically done after a rigid dynamics simulation is used to verify the model set-up, a flexible dynamics simulation can provide information about machine performance such as:Will a machine or mechanism work adequately with light, more flexible members, or will stiffer, but heavier members be required?Will the forces transmitted through joints exceed the strength of the materials being used?At what rotational or translation speed will the mechanism experience plastic deformation and begin to fail?Will the mechanism’s natural frequencies be ex cited and lead to instability?Will the repeated loading/unloading lead to fatigue, and if so, where?A Flexible Dynamics simulation can be performed using ANSYS Structural, Mechanical, or Multiphysics products.> 2. Reliability, Availability & Maintainability Analysis3. Fatigue AnalysisThe ANSYS Fatigue Module adds the capability to simulate performance under anticipated cyclic loading conditions over a product's anticipated life span. Incorporating both Stress Life and Strain Life analyses with a variety of mean stress correction methods, including Morrow, Smith-Watson-Topper (SWT) and no mean effects, the Fatigue Module provides contour plots of fatigue life, damage, factor of safety and stress biaxiality. Additional results include rainflow matrix, damage matrix, fatigue sensitivity and hysteresis.For Stress Life the fatigue module supports the following fatigue types:Constant amplitude, proportional loadingNon-constant amplitude, proportional loadingConstant amplitude, non-proportional loadingFor Strain Life the fatigue module supports the following fatigue types:Constant amplitude, proportional loadingNon-constant amplitude, proportional loadingFatigue Module contour plot of fatigue life and safety.4. High Altitude Analysis>> 5. Control Loop Analysis>> 6. Electromagnetic Compatibility (EMC) Analysis >> 7. Packing & Shipping Analysis。

ResearchPaper-IJMERR

ResearchPaper-IJMERR

119This article can be downloaded from /currentissue.phpSIMULATION STUDIES ON THE EFFECT OF PROJECTILE NOSE SHAPE IMPACTING ON ALUMINUM PLATESSivaiah A 1*, Nageshwar Reddy V 1 and Syed Altaf Hussain 1*Corresponding Author:Sivaiah A, ***********************In mechanics, an impact is a high force or shock applied over a short period when two or more bodies collide. Such a force or acceleration usually has a greater effect than a lower force applied over a proportionally longer period of time. The effect depends critically on the relative velocity of the bodies to one another. Structural failure due to impact is a common but complex phenomenon. In earlier days the impact problems were primarily confined to the military. As the civilian technology has grown in sophistication, more studies are being carried out to understand the behavior of materials subjected to short duration of loading. The field of impact dynamics is of interest to engineers concerned with design of light weight body amour, safety of nuclear-reactor containment vessels subjected to missile or aircraft impact, protection of spacecraft from meteoroid impact, safe demolition of pre stressed concrete structures and transportation safety of the hazardous materials. In the present work, simulation is performed by impacting aluminum plates of three different thicknesses viz. 0.81 mm, 1.51 mm and 2.05 mm by three different nose projectiles, i.e., blunt, conical and hemispherical with varying kinetic energy in Finite Element Code. Problem is modeled using ANSYS/Explicit Axi-symmetric Model.Keywords:Impact, Projectile velocity, Impact velocity, Residual velocity, Velocity drop INTRODUCTIONIn earlier days, the impact problems wereprimarily confined to the military. As the civiliantechnology has grown in sophistication, morestudies are being carried out to understandthe behavior of materials subjected to shortdynamics is of interest to engineers concerned with design of light weight body amour, safety of nuclear-reactor containment vessels subjected to missile or aircraft impact,protection of spacecraft from meteoroid impact, safe demolition of pre-stressed concrete structures and transportation safety Research Paper120This article can be downloaded from /currentissue.php Impact could be defined as collision of twobodies. The intensity of impact couldbe assmall as the hit of a droplet of rainwater onearth and as high as the collision of twoheavenly bodies such as comets or asteroids.In mechanics, an impact is a high force orshock applied over a short period when twoor more bodies collide. Such a force oracceleration usually has a greater effect thana lower force applied over a proportionallylonger period of time. The effect dependscritically on the relative velocity OBJECTIVE OF THE PROJECT In the present work numerical simulations areperformed on thin aluminium plates of threethicknesses 0.81 mm, 1.51 mm and 2.05 m,subjected to impact by conical, hemispherical and blunt projectiles. Projectiles are impacted normally with velocities in the sub-ordinance range.In modelling the problem in ABAQUS, effect of number of elements on the plate and type of element (triangular, quad) for different projectiles is studied.Impact and residual velocities are measured and energy absorbed by the projectile is calculated. Thicknesses of the plates and impact velocity of the projectile are varied. Mass anddimensions of the projectile are kept constant.Impact velocity is related to the residual velocityand velocity drop. Also variation of absorbedenergy with impact energy is studied.MODELLING OF THE PROBLEM121This article can be downloaded from /currentissue.php distortion in case of conical nosed projectile.For the case of impact by blunt and hemispherical nosed projectiles, quadrilateral elements were employed. An impact zone was created, where the projectile comes in contact with the plate, in which the mesh density was higher and was reduced as the distance from the impact area increased. The aspect ratio of the elements in the impact zone was maintained as unity; however it was allowed to increase elsewhere.Meshing StrategyThe target plate for the case of conical andhemispherical nosed projectiles was modelledwith continuum solid axisymmetric triangular3 noded elements with single integration point.This was done in order to reduce element122This article can be downloaded from /currentissue.php ABACUS INTRODUCTIONTable 4: Number of Elements Along the Thickness in MeshingFigure 5: Step 2 – PlateFigure 6: Step 3 – Entering the Material Properties, Inertia, Boundary Condition for the Figures123This article can be downloaded from /currentissue.php RESULTSFigure 6: Vonmises Stress Contour for Blunt Materials Figure 7: Vonmises Stress Contour for Blunt and Conical MaterialsFigure 9: Vonmises Stress Contour Hemi Spherical Materials Table 5: Residual VelocityBluntConicalHemi Spherical124This article can be downloaded from /currentissue.php CONCLUSION The present study deals with numericalsimulation of normal impact of projectile on thinsingle layered aluminium plates usingcommercial finite element code ABAQUS.Aluminium Plates are subjected to impact bythree different projectiles having conical,hemispherical and blunt noses. Impact andresidual velocities are obtained from the finiteelement code and impact and absorbedenergies are then calculated. The deformationmechanisms resulting from different noseshapes are also studied.Table 5: Velocioty DropBluntConicalHemi125This article can be downloaded from /currentissue.php In case of conical and hemisphericalprojectile the mode of deformation is petalling.They cause failure in the target by ductile holeenlargement. The nose of the projectile firstmade a minute hole in the target along the axisof the trajectory of the projectile and deformedthe target at the centre in shape of crater aroundthe nose of the projectile. In blunt projectileimpact a circular plug of diameter equal to thatof projectile is removed from the plate. Thethickness of plug is found to be same as that ofthe plate. As soon as the projectile comes incontact with the plate a global deformation inform of dishing takes place. The target platekeeps on deforming until the compressive forceapplied by the blunt projectile equals the plasticshear stress of the plate material and shearingof a plug takes place.It is observed from graph of residualvelocities that they follow a quadratic curve;conical projectile penetrated the target moreeasily than the hemispherical and bluntprojectiles, as is evident from the fact that forthe same impact velocity the residual velocityobtained for conical projectile case is more.The residual velocities were found to decreasewith increase in plate thickness for all blunt,conical and hemispherical projectiles.For the same thickness the energyabsorbed by target plate in case ofhemispherical projectile is highest. In case ofconical projectile energy absorbed is lowestand for blunt it lies after hemispherical. Forsame amount of impact energy (164 J) theenergy absorbed by 1.51 mm plate forhemispherical projectile case is around 66.06J and for conical projectile it is 27.63 J. Forthe same impact energy, energy absorbed byblunt projectile is 35.9 J. The absorbedenergies were found to increase with plate thickness; this increment was higher in case of hemispherical projectiles.The velocity drop of projectiles was found to increase with plate thickness, as the velocity is increased the drop in velocity decreases for same thickness and follows a quadratic trend line.REFERENCES 1.Bÿrvik T, Langseth M, Hopperstad O S and Malo K A (2002a), “Perforation of 12mm Thick Steel Plates by 20 mm Diameter Projectiles with Flat,Hemispherical and Conical Noses Part I:Experimental Study”,Int. J. of Impact Engg., Vol. 27, pp. 19-35.2.Bÿrvik T, Langseth M, Hopperstad O S and Malo K A (2002b), “Perforation of 12mm Thick Steel Plates by 20 mm Diameter Projectiles with Flat,Hemispherical and Conical Noses Part II:Numerical Simulations”,Int. J. of Impact Engg., Vol. 27, pp. 37-64.3.Chen X W and Li Q M (2003), “Shear Plugging and Perforation of Ductile Circular Plates Struck by a Blunt Projectile”,Int. J. of Impact Engg., Vol. 28,pp. 513-536.4.Gupta N K, Iqbal M A and Sekhon G S (2008), “Effect of Projectile Nose Shape,Impact Velocity and Target Thickness on the Deformation Behaviour of Layered Plates”,Int. J. of Impact Engg., Vol. 35,pp. 37-60.5.Gupta N K, Ansari R and Gupta S K(2001), “Normal Impact of Ogive Nosed126This article can be downloaded from /currentissue.php Projectile on Thin Plates”,Int. J. of ImpactEngg., Vol. 25, pp. 641-660.6.Iqbal M A, Chakrabarti A and Gupta N K(2010), “3D Numerical Simulations of Sharp Nosed Projectile Impact on Ductile Targets”,Int. J. of Impact Engg., Vol. 37,pp. 185-195.。

倪以信动态电力系统PowerSystemDynamics

倪以信动态电力系统PowerSystemDynamics

Introduction (5)
0.4 Definitions of different types of P. S. stability
P. S. stability: the property of a P. S. that enable it to remain in a state of operating equilibrium under normal operating conditions and to return to an acceptable state of equilibrium after being disturbed.
* S. M. is a rotating magnetic element with complex dynamic behavior. It is the heart of P. S. It
* It provides active and reactive power to loads and has strong power, frequency and voltage regulation/control capability .
The time span considered:
transient stability: 0 to 10 seconds mid-term stability: 10 seconds to a few minutes long-term stability(dynamics): a few minutes to 1 hour
1.1.1 Ideal S. M. definition (cont.):
Assumptions for ideal S. M. Machine magnetic permeability (m) is a constant with magnetic saturation neglected. Eddy current, hysteresis, and skin effects are neglected, so the machine is linear.

叉型分岔和鞍点分岔的区别

叉型分岔和鞍点分岔的区别

叉型分岔和鞍点分岔的区别英文回答:Bifurcation is a phenomenon in dynamical systems wherea small change in a parameter leads to a qualitative change in the system's behavior. There are different types of bifurcations, including pitchfork bifurcation and saddle-node bifurcation.Pitchfork bifurcation, also known as fork bifurcationor cusp bifurcation, occurs when a stable equilibrium point splits into two stable points and an unstable point as a parameter is varied. This creates a "fork" shape in the bifurcation diagram. It is called pitchfork bifurcation because the diagram resembles the shape of a pitchfork. Pitchfork bifurcation is a common occurrence in symmetric systems.For example, let's consider a simple model ofpopulation dynamics. Suppose we have a predator-prey system,where the predator population depends on the prey population. As the prey population increases, the predator population also increases. However, at a certain point, the predator population becomes too large, leading to a decline in the prey population, which in turn causes the predator population to decrease. This creates a stable equilibrium point where both populations coexist. Now, if we gradually increase the availability of resources, such as food, for the prey, we may reach a point where the stable equilibrium point splits into two stable points and an unstable point. This bifurcation represents a qualitative change in the system's behavior, as it transitions from a stable coexistence of predator and prey to a situation where one population dominates over the other.On the other hand, saddle-node bifurcation, also known as fold bifurcation or tangential bifurcation, occurs when two equilibrium points collide and annihilate each other as a parameter is varied. This creates a "saddle" shape in the bifurcation diagram. It is called saddle-node bifurcation because the diagram resembles the shape of a saddle. Saddle-node bifurcation is a common occurrence in systemswith bistability.Let's consider a simple example of a chemical reaction. Suppose we have a reaction where two reactants can form two different products. At low concentrations of the reactants, one product dominates, while at high concentrations, the other product dominates. There is a parameter, such as temperature or pressure, that determines which product is favored. As we vary this parameter, we may reach a point where the two equilibrium points corresponding to the two products collide and disappear. This bifurcation represents a qualitative change in the system's behavior, as it transitions from a situation where one product dominates to a situation where only one product is formed.中文回答:英文回答:分岔是动力系统中的一种现象,当参数的微小变化导致系统行为的性质变化。

双马赫—曾德型光纤周界安防系统的算法研究及其实现

双马赫—曾德型光纤周界安防系统的算法研究及其实现

摘要随着光纤传感技术的飞速发展,基于双马赫-曾德干涉型振动传感器的光纤周界安防监测技术应运而生。

目前光纤周界安防难以实现长距离条件下精确定位,且同时高效地识别多种入侵行为。

为了降低长距离监测的定位误差并且得到更加具体的扰动信息,本文重点研究了分布式全光纤智能周界安防系统的长距离定位和模式识别算法,在优化系统性能的基础上完成了算法开发。

本文在介绍光纤周界安防技术的研究现状、分析其尚存不足之处的基础之上,重点开展了以下几个方面的研究工作:1.介绍了分布式光纤传感技术,研究了双马赫-曾德型光纤周界安防系统的传感和定位原理,分析了长距离定位检测和对入侵事件进行模式识别的意义。

2.基于长距离双马赫-曾德干涉传感理论模型及其工作原理,分析了该系统中定位精度的影响因素,基于经验模态分解(Empirical Mode Decomposition)方法优化并完善了长距离定位算法,利用实际实验验证和分析了该算法的有效性。

3.采用峭度估计、经验模态分解和径向基函数神经网络,开发了结合EMD 和RBF(Radial Basis Function)的高效率多事件模式识别方法,通过算法的模拟仿真分析验证了该算法的可行性。

4.基于Visual Studio 2010平台,利用模块化设计思想实现了系统相关算法及控制软件。

通过实验对系统进行性能测试,验证该系统运行的长期稳定性,并对安防区域进行准确定位、实时报警及全天候地视频监控。

关键词:光纤振动传感,马赫-曾德干涉仪,定位算法,模式识别,交互界面设计ABSTRACTWith the rapid development of optical fiber sensing technology, optical fiber perimeter security monitoring technology based on Dual Mach-Zehnder interference vibration sensor came into being. Currently the optical fiber perimeter security system is difficult to achieve positioning accurately in the long range, and at the same time it can not identify various intrusions efficiently. In order to reduce the positioning error of the system in the long range monitoring and obtain more specific information of the disturbance, this paper focuses on positioning algorithm and pattern recognition algorithms in all fiber distributed intelligent perimeter security system, and completes the algorithm development on the basis of optimizing the system performance.This paper focus on the following aspects of the research work based on introducing the status quo of the fiber perimeter security technology and analyzing the remaining deficiencies:1. We introduce the distributed optical fiber sensing technology and study the sensing and positioning principle of the Dual Mach-Zehnder fiber perimeter security system. Besides, we analyze the significance of long-range location detection and pattern recognition for intrusion events.2. Based on the Dual Mach-Zehnder interference sensing theory model and its working principle in the long distance, we analyze the influence factors of positioning accuracy in this system. And then we optimize and perfect the localization algorithm in the long distance on the basis of the empirical mode decomposition method (EMD). Furthermore, the effectiveness of the algorithm is analyzed and verified by practical experiments.3. A high-efficiency multiple events discrimination method combining EMD and RBF (Radial Basis Function) is developed by using kurtosis estimation, empirical mode decomposition and radial basis function neural network. We analyze the feasibility of the algorithm through the simulation.4. We use the modular design idea to realize the system-related algorithms and control software based on the Visual Studio 2010 platform. In order to verity the long-term stability of the system, we have conducted in-field experiments to test the performance of the system. Besides, the intrusion is accurately located, real-timealarmed and video surveillance is made all-weather in the security area.KEY WORDS: Fiber vibration sensing, Mach-Zehnder interferometer, Positioning algorithm, Pattern recognition, Interactive interface design目录摘要 (I)ABSTRACT ......................................................................................................... I I 目录 (IV)第1章绪论 (1)1.1课题的背景和意义 (1)1.2 光纤传感技术在周界安防中的应用 (2)1.3事件定位与模式识别的意义 (6)1.4 本论文的主要工作 (7)第2章光纤周界安防系统的理论研究 (9)2.1系统的传感原理 (9)2.1.1马赫-曾德干涉仪传感原理 (9)2.1.2 双马赫-曾德干涉仪结构传感原理 (11)2.2系统的扰动定位原理 (12)2.2.1 系统传感光路的构成 (12)2.2.2时延差计算法 (13)2.3系统硬件的构成及实现 (13)2.4 系统软件的设计 (17)2.5 本章小结 (18)第3章定位算法研究 (19)3.1系统定位算法理论分析 (19)3.1.1非对称双马赫-曾德传感模型 (19)3.1.2基于过零率的端点检测 (20)3.1.3改进的EMD算法 (21)3.1.4基于互相关的时延估计 (22)3.2 影响定位性能的因素分析 (23)3.3长距离定位算法的验证 (24)3.4本章小结 (28)第4章模式识别算法研究 (29)4.1 模式识别算法理论分析 (29)4.1.1 经验模态分解EMD理论分析 (29)4.1.2峭度的理论分析 (31)4.1.3 径向基函数神经网络RBF理论分析 (32)4.2 模式识别的方法 (34)4.2.1 聚类分析法 (34)4.2.2 支持向量机分类法 (35)4.2.3 神经网络分类法 (36)4.3 高效率多事件的模式识别算法的实验验证 (37)4.4本章小结 (41)第5章界面分析与系统实验 (43)5.1 Visual Studio 2010平台和C#简介 (43)5.2 光纤周界安防系统软件平台的设计 (44)5.2.1采集模块 (45)5.2.2偏振控制模块 (46)5.2.3入侵判定模块 (46)5.3系统数据库设计 (48)5.3.1 MySQL数据库的简介 (48)5.3.2数据表的设计 (49)5.4 UI界面分析 (49)5.4.1菜单栏 (50)5.4.2 工具栏 (51)5.4.3子窗体显示界面 (51)5.5系统性能指标 (58)5.6本章小结 (59)第6章总结与展望 (60)参考文献 (62)发表论文和参加科研情况说明 (68)致谢 (70)第1章绪论1.1课题的背景和意义近年来,伴随着社会的发展和科技的进步,尤其是信息时代的来临,高新科技不断发展创新,但是科技是把双刃剑,发达的科技同时也使犯罪分子的非法入侵手段更加隐蔽化、复杂化和智能化,因此人们的安防意识需要不断增强,安全防范技术需要不断提高。

大气动力学中三种Rossby波作用通量的特征差异和适用性比较

大气动力学中三种Rossby波作用通量的特征差异和适用性比较

大气动力学中三种Rossby波作用通量的特征差异和适用性比较施春华;金鑫;刘仁强【摘要】大气动力学诊断Rossby波的传播时,通常用波作用通量来表示.常用的三种波作用通量分别为Plumb波作用通量,T-N波作用通量和局地E-P通量.本文详细讨论了这三种方法的特征差异,并结合2016年1月的一次寒潮事件,比较了三种方法在该事件中的适用性.结果表明:1)Plumb波作用通量的纬向分量较大而经向分量较小,适用于振幅较小的纬向均匀的西风带Rossby长波的诊断.2)T-N波作用通量是对Plumb波作用通量的改进,经向分量得以增强,能更好地描述纬向非均匀气流中的较大振幅的西风带Rossby长波扰动.T-N波作用通量计算时,背景场取多年平均的当月气候场较合适,能更好地反映当前季节内的Rossby波传播异常.3)局地E-P通量可以诊断一段时间内天气尺度瞬变波对背景场(定常波)总的调控作用,但无法直接反映Rossby长波的逐时演变(T-N波或Plumb波作用通量则可以).%Plumb wave activity flux,T-N wave activity flux and local E-P wave activity flux are widely used to analyze the propagation of Rossby wave in atmospheric dynamics.The differences in characteristics and applicability among three types of Rossby wave activity fluxes are discussed in a case study of a cold wave in January 2016.Plumb wave activity flux with strong zonal component and weak meridional component is suitable for the analysis of Rossby waves with small amplitude in the zonally symmetric westerly.T-N wave activity flux with improved meridional component based on Plumb wave activity flux is appropriate for analyzing Rossby waves in the zonally asymmetric westerly.T-N wave activity flux derived onthe multi-year average climatic field of current month canmore successfully indicate wave propagation anomaly in current season.Local E-P wave activity flux can illustrate the modulating effect of transient waves on background field (stationary waves),but can not reflect the evolution of long waves.【期刊名称】《大气科学学报》【年(卷),期】2017(040)006【总页数】6页(P850-855)【关键词】Rossby波;局地E-P通量;Plumb波作用通量;T-N波作用通量【作者】施春华;金鑫;刘仁强【作者单位】南京信息工程大学气象灾害教育部重点实验室/气象灾害预报预警与评估协同创新中心,江苏南京210044;南京信息工程大学气象灾害教育部重点实验室/气象灾害预报预警与评估协同创新中心,江苏南京210044;南京信息工程大学气象灾害教育部重点实验室/气象灾害预报预警与评估协同创新中心,江苏南京210044【正文语种】中文Elisassen-Palm(E-P)通量在经向—垂直剖面上能有效诊断Rossby波传播及其与纬向基本气流相互作用(Anderws and McIntyre,1976,1978)。

CED-1.3

CED-1.3

Chapter 1
Review
In last two sections, we obtained two set vector partial differential equations for electrostatics and magnetostatics, respectively.
They seam to be the independent theories.
Chapter 1
For static electric field is conservative field, the closed line integral for it is vanished.
Faraday’s Law the non-conservation EMF field is produced in a closed circuit if the magnetic flux through this circuit varies with time.
Aug 26, 2004
Classical Electrodynamics
Jingbo Zhang
Section 3 Eletrodynamics
3 Faraday’s Law of Induction
Ohm’s Law and Electromovtive Force
Chapter 1
Under certain physical conditions, and for certain materials, there is a linear relationship between the current density and electric Field,
The electric charge conservation law can be formulated in the equation of continuity,

复杂等离子体晶格中的低频模

复杂等离子体晶格中的低频模

off'’iS seen at the long wavelength end of the dispersion.
or、析tll the screened Coulomb interaction between a charged dust and particles in the nearest eight cubic only being taken into account(screening parameter必">>1).We then discuss the effects of screening parameters on the dispersion relations of DLW.
and complex plasma crystals has been made. In the second chapter,we discuss the dispersion relations of DLW in complex plasma
crystals systematically,propose the concept of dispersion relation matrix of DLW in complex plasma crystals,derive the dispersion relation matrices for DLW in body centred cubic(bcc) and face centred cubic(fee)in three—dimensional complex plasma crystals,and obtain the simple forms of the dispersion relation matrices of DLW in the three characteristic directions ((1,0,0),(1,1,O)and(1,1,1)).We compute the dispersion relation matrices晰th the screened Coulomb interaction between a charged dust and all other particles being taken into account

扩散系数总结

扩散系数总结

1.离子液体在其他溶剂中的扩散系数7. 五种1-乙基-3-甲基咪唑型离子液体在水溶液中无限稀释,温度范围303.2-323.2K下的扩散系数Taylor dispersion method9. 甲醇/[BMIM][PF6]体系中,25℃下不同[BMIM][PF6]浓度的相互扩散系数42. [C4C1im]BF4, [C4C1im][N(OTf)2],[C4C1im]PF6三种离子液体在甲醇,CH2Cl2中的扩散系数2.其他物质在离子液体中的扩散系数2.1 具有氧化还原活性的分子在离子液体中的扩散系数5. 水在离子液体[BMIM][TFSI] 中的反常扩散6. 三碘化物在混合离子液体中的扩散系数MPII,EMIC,EMIDCA,EMIBF4,EMINTf2 14. CO,DPA,DPCP在不同离子液体中的扩散系数17.CO2在离子液体中的扩散系数41.气体在[BMIM][PF6]中的扩散系数和离子液体的自扩散系数20. 气体在五种鏻型离子液体中的扩散系数21. 25℃下三碘化物在两种离子液体混合物中的扩散系数43 1,1,1,2-tetrafluoroethane (R-134a)在七种离子液体中的扩散系数3.离子液体的自扩散系数3.1 1-ethyl-3-methylimidazolium tetrafluoroborate ([emim][BF4]) 和LiBF4混合Li BF4六种不同浓度下离子的自扩散系数3. EMIBF4,EMITFSI,BPBF4,BPTFSI中阳离子和阴离子的自扩散系数4. 咪唑型离子液体分子动力学模拟自扩散8. [BMIM][PF6] (自制和购买两种)在不同温度下的自扩散系数10. 胍基型离子液体的自扩散研究模型11. [bmim][PF6]的分子动力学研究12.N-methyl-N-propyl-pyrrolidinium bis-(trifluoromethanesulfonyl)imide (PYR13TFSI)和LiTFSI混合体系中不同温度和组成下离子的自扩散系数13.(1− x)(BMITFSI), x LiTFSI x<0.415. 质子传递的离子液体的自扩散系数16. DEME-TFSA 和DEME-TFSA-Li 的自扩散系数18 用pulsed field gradient NMR测离子液体和离子液体混合物的传递性质41.气体在[BMIM][PF6]中的扩散系数和离子液体的自扩散系数25. 离子液体不同侧链长度对扩散的影响1. 离子液体在其他溶剂中的扩散系数2. 其他物质在离子液体中的扩散系数2.1 具有氧化还原活性的分子在离子液体中的扩散系数离子液体1-butyl-3-methylimidazolium bis-(trifluoromethylsulfonyl)amide [BMIM][TFSI] butyltriethylammonium bis(trifluoromethylsulfonyl)amide) [Et3BuN][TFSI]N-methyl-N-butylpyrrolidinium bis{(trifluoromethyl)sulfonyl}-amide [Pyr][TFSI]被测的氧化还原对Dodzi Zigah, Jalal Ghilane, Corinne Lagrost, and Philippe Hapiot .Variations of diffusion coefficients of redox active molecules in room temperature ionic liquids upon electron transfer. J. Phys. Chem. B, 2008, 112 (47), 14952-149583. 离子液体的自扩散系数3.1 1-ethyl-3-methylimidazolium tetrafluoroborate ([emim][BF4]) 和LiBF4混合Li BF4六种不同浓度下离子的自扩散系数Fig.1 Arrhenius plots of the self-diffusion coefficients for (a) Li, (b) BF4, and (c) [emim].在[emim][BF4]中,尽管[emim]分子大小比[BF4]大,但是[emim]扩散比[BF4]稍微快一点,说明[BF4]不是以单个离子扩散的。

Matlab中LMI(线性矩阵不等式)工具箱使用例子

Matlab中LMI(线性矩阵不等式)工具箱使用例子

Matlab中LMI(线性矩阵不等式)⼯具箱使⽤例⼦这⼀段被⽼板逼着论⽂开题,⾃⼰找⽅向⽐较着急,最后选择了供应链控制理论的⼀个⽅向。

我要写的论⽂,⽤到了Matlab 的LMI⼯具,以及某篇论⽂中的H-inf稳定定理。

⾃⼰好好研究了好长时间,怎么也⽆法实现该论⽂当中的算例。

研究了⼀个多⽉,⾃⼰简直就快崩溃了,也搞不定问题。

我很是怀疑⾃⼰的选题是不是正确,并且怀疑⾃⼰是不是选的太难了。

如果连论⽂中的算例都⽆法实现,如何把该模型应⽤到⾃⼰论⽂当中呢?功夫不负有⼼⼈,昨⽇我加⼊了Mathworks的Matlab的Newsgroup,结果碰见⼀⽜⼈Johan,⽴即就把论⽂中的算例给写成程序。

但是他做出的结果和论⽂仍然有差别,我仍有点不⽢⼼,⼈家的论⽂发表在Automatica上,如果连这种期刊都⽔的要命,那么就没有什么学术⽔平了。

今天中午,仍然不⽢⼼,⽼爸给我打了电话让我看红场阅兵,于是我边看PPMate边漫⽆边际的核对着⾃⼰的程序。

终于做出了和算例⼀致的结果。

我搜出来的都是⼀些简单的算例,并且机会没有中⽂教程,我在这⾥就⽃胆把⾃⼰的体会写出来,试着给⼤家提供⼀点参考。

LMI:Linear Matrix Inequality,就是线性矩阵不等式。

在Matlab当中,我们可以采⽤图形界⾯的lmiedit命令,来调⽤GUI接⼝,但是我认为采⽤程序的⽅式更⽅便(也因为我不懂这个lmiedit的GUI)。

对于LMI Lab,其中有三种求解器(solver): feasp,mincx和gevp。

每个求解器针对不同的问题:feasp:解决可⾏性问题(feasibility problem),例如:A(x)<b(x)。

< font="">mincx:在线性矩阵不等式的限制下解决最⼩化问题(Minimization of a linear objective under LMI constraints),例如最⼩化c'x,在限制条件A(x) < B(x)下。

薛定谔培训教程

薛定谔培训教程

Accurate Docking
Pose Refinement
ห้องสมุดไป่ตู้
SP_Glide
XP_Glide
~30s/ligand 5 – 10 min/ligand
高通量虚拟筛选 Deposited in PDB (hydrogens added)
No other nearby acceptor atoms for Ser
– National Academy of Sciences and recipient of the Priestley Medal from the ACS – Synthetic and mechanistic organic chemist with focus on anti-cancer drugs
Refined by PrimeX
2.95 Å
2.67 Å
1XOZ (Resolution = 1.37 Å)
高通量虚拟筛选
1qpe top ranked active site
• White balls are site points which represent available volume in the active site General hydrophobic volumes are in yellow Hydrophilic h-bond acceptor and donor volumes are in blue and red Additional surfaces include
• Barry Honig - Professor, Department of Biochemistry and Biophysics, Columbia University

常微分方程与动力系统青年研讨会

常微分方程与动力系统青年研讨会

常微分方程与动力系统青年研讨会2019.4.12-4.141.会议日程 (2)2.报告摘要 (4)上海交通大学数学科学学院&教育部科学工程计算重点实验室1.会议日程4.13 报告报告人8:25-8:30 开幕式:肖冬梅主持人:肖冬梅8:30-9:00 Variational formulations and stability of steady equatorial waves with储继峰vorticity9:00-9:30 关于近完全可积系统的一些研究结果吴昊9:30-10:00 On several Lotka-Volterra competitive systems 周鹏10:00-10:20 茶歇主持人:于江10:20-10:50 Global dynamics of a cubic Lienard system 陈和柏10:50-11:20 The stability of full dimensional KAM tori for nonlinear Schrödinger丛洪滋equation11:20-11:50 Bifurcations of limit cycles around the boundaries of a period annulus 田云11:50-13:45 午餐主持人:储继峰13:45-14:15 The limit distribution of inhomogeneous Markov processes andKolmogorov's problem 柳振鑫14:15-14:45 Time-Domain Analysis of an Acoustic–Elastic Interaction Problem 高忆先14:45-15:15 Long time stability of Hamiltonian partial differential equations withderivatives in nonlinearities 张静15:15-15:45 Invariant Cantor manifolds of quasi-periodic solutions for the DNLSequation 高美娜15:45-16:00 茶歇主持人:柳振鑫16:00-16:30 双曲之外微分动力系统的一些遍历理论进展田学廷16:30-17:00 C^1-openness of non-uniform hyperbolic diffeomorphisms withbounded C^2 norm 杨佳刚17:00-17:30 The mixing property of partially hyperbolic attractors 杨大伟17:30-18:00 Werk KAM solutions and twist maps of the annulus MaximeZavidovique 18:00-20:00 晚餐4.14 报告报告人主持人:杨大伟8:45-9:15 微分动力系统中的内蕴持续动力学行为与双曲性文晓9:15-9:45 Hyperbolicity vs. non-hyperbolic ergodic measures inside homoclinic王晓东classes9:45-10:10 茶歇主持人:文晓10:10-10:40 Dynamics and bifurcations of some piecewise smooth differential唐异垒systems10:40-11:10 Weak KAM Theory and its Applications 王楷植11:10-11:30 讨论11:30-12:30 午餐2.报告摘要Global dynamics of a cubic Lienard system陈和柏(福州大学)Abstract:In this talk, we investigate the dynamical behaviour of a cubic Liénard system with global parameters. For global parameters we give a positive answer to conjecture 3.2 of (1998 Nonlinearity 11 1505–19) about the existence of some function whose graph is exactly the surface of double limit cycles.Variational formulations and stability of steady equatorial waves with vorticity储继峰(上海师范大学)Abstract:When the vorticity is monotone with depth, we present a variational formulation for steady periodic water waves of the equatorial flow in the $f$-plane approximation, and show that the governing equations for this motion can be obtained by studying variations of a suitable energy functional $\mathcal{H}$ in terms of the stream function and the theromcline. We derive criteria which ensure that the second variation of the constrained energy functional is a nonnegative form, proving thus linear stability of steady equatorial water waves with vorticity.The stability of full dimensional KAM tori for nonlinear Schrödinger equation丛洪滋(大连理工大学)Abstract:In this talk,we will discuss the existence and long time stability the full dimensional invariant tori for 1D nonlinear Schrödinger equation with periodic boundary conditions.Invariant Cantor manifolds of quasi-periodic solutions for the DNLS equation高美娜(上海第二工业大学)Abstract:We are concerned with the derivative nonlinear Schrodinger equation with periodic boundary conditions. We show the above equation possesses Cantor families of smoothquasi-periodic solutions of small amplitude. The proof is based on an infinite dimensional KAM theorem for unbounded perturbation vector fields.Time-Domain Analysis of an Acoustic–Elastic Interaction Problem高忆先(东北师范大学)Abstract:Consider the scattering of a time-domain acoustic plane wave by a bounded elastic obstacle which is immersed in a homogeneous air or fluid. This paper concerns the mathematical analysis of such a time-domain acoustic–elastic interaction problem. An exact transparent boundary condition (TBC) is developed to reduce the scattering problem from an open domain into an initial-boundary value problem in a bounded domain. The well-posedness and stability are established for the reduced problem. A priori estimates with explicit time dependence are achieved for the pressure of the acoustic wave field and the displacement of the elastic wave field. Our proof is based on the method of energy, the Lax–Milgram lemma, and the inversion theorem of the Laplace transform. In addition, a time-domain absorbing perfectly matched layer (PML) method is introduced to replace the nonlocal TBC by a Dirichlet boundary condition. A first order symmetric hyperbolic system is derived for the truncated PML problem. The well-posedness and stability are proved. The time-domain PML results are expected to be useful in the computational air/fluid–solid interaction problems.The limit distribution of inhomogeneous Markov processes and Kolmogorov's problem柳振鑫(大连理工大学)Abstract:In this talk, we will talk about the limit distribution of inhomongeneous Markov processes, especially those generated by the SDEs. Meantime, we will also discuss the recent progress in Kolmogorov's problem on the limit behavior of stationary distributions of diffusion processes as the diffusion tends to zero.Dynamics and bifurcations of some piecewise smooth differential systems唐异垒(上海交通大学)Abstract:In this talk, we study the dynamics and the bifurcations of some piecewise smooth differential systems and exhibit rich and complicated dynamical phenomena, such as Hopfbifurcation, grazing bifurcation, grazing-sliding bifurcation and bifurcations of limit cycles. All global phase portraits of the system are presented on the Poincar\'e disc.双曲之外微分动力系统的一些遍历理论进展田学廷(复旦大学)Abstract:一方面介绍Bowen针对双曲之外提出的统计式理论及Specificaition存在性问题在非一致双曲系统情形的进展,例如发现了多种Specification新形式(较原Specification虽然失去了很多一致性,但跟踪程度指数式变化、相邻回复时刻几乎无间隙等新观察弥补了缺陷)并可用于得到Poincare回复时刻与Lyapunov指数的关系、时间平均饱和集的存在性及其拓扑熵与对应测度熵的变分原理并应用于重分形理论(适用于Bonatti-Viana、Mañé、Katok等发现的几大类双曲之外的系统);另一方面在Specification对遍历平均的应用上有一些新进展(在一致双曲时也是新的),例如肯定Mañé关于Oseledec乘法遍历定理中Lyapunov正则性的拓扑论断、得到回复轨道层次的满拓扑熵和分布混沌等描述。

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a rX iv:c ond-ma t/16242v1[c ond-m at.dis-nn]13J un21Local field dynamics in symmetric Q -Ising neural networks D.Boll´e ∗†Instituut voor Theoretische Fysica,K.U.Leuven,B-3001Leuven,Belgium and G.M.Shim ‡Department of Physics,Chungnam National University Yuseong,Taejon 305-764,R.O.Korea Abstract The time evolution of the local field in symmetric Q -Ising neural networks is studied for arbitrary Q .In particular,the structure of the noise and the appearance of gaps in the probability distribution are discussed.Re-sults are presented for several values of Q and compared with numerical simulations.Key words:Symmetric networks;Q -Ising neurons;parallel dynamics;local field;probabilistic approach1IntroductionIn a number of papers in the nineties(cfr.[1]-[10]and references therein)the parallel dynamics of Q-Ising type neural networks has been discussed for several architectures–extremely diluted,layered feedforward,recurrent–using a proba-bilistic approach.For the asymmetric extremely diluted and layered architectures the dynamics can be solved exactly and it is known that the localfield only con-tains Gaussian noise.For networks with symmetric connections,however,things are quite different.Even for extremely diluted versions of these systems feedback correlations become essential from the second time step onwards,complicating the dynamics in a nontrivial way.A complete solution for the parallel dynamics of symmetric Q-Ising networks at zero-temperature taking into account all feedback correlations,has been ob-tained only recently using a probabilistic signal-to-noise ratio analysis[9]-[10]. Thereby it is seen that both for the fully connected and the extremely diluted symmetric architectures,the localfield contains a discrete and a normally dis-tributed noise part.The difference between the two architectures is that for the diluted model the discrete part at a certain time t does not involve the spins at all previous times t−1,t−2,...up to0but only the spins at time step t−1.Even so, this discrete part prevents a closed-form solution of the dynamics but a recursive scheme can be developed in order to calculate the complete time evolution of the order parameters,i.e.,the retrieval overlap and the activity.In the work above the focus has been on the non-equilibrium behavior of the order parameters of the network.But,since the localfield itself is a basic in-gredient in the development of the relevant recursive scheme it is interesting to study also the non-equilibrium behavior of the localfield distribution.The more so since this distribution does not convergence to a simple sum of Gaussians as is frequently thought,but it develops a gap structure.This is precisely one of the points studied in detail in the present communication.Moreover,the analogies and differences between the fully connected architecture and the symmetrically diluted one are highlighted.Finally,numerical simulations are presented confirm-ing the analytic study and giving additional insight in the structure of these local field distributions.2The modelConsider a neural networkΛconsisting of N neurons which can take values σi from a discrete set S={−1=s1<s2<...<s Q=+1}.The p patternsto be stored in this network are supposed to be a collection of independent and identically distributed random variables(i.i.d.r.v.),{ξµi∈S},µ∈P={1,...,p} and i∈Λ,with zero mean,E[ξµi]=0,and variance A=Var[ξµi].The latter is a measure for the activity of the patterns.Given the configurationσΛ(t)≡{σj(t)},j∈Λ={1,...,N},the localfield in neuron i equalsh i(σΛ(t))= j∈ΛJ ij(t)σj(t)(1)with J ij the synaptic coupling from neuron j to neuron i.In the sequel we write the shorthand notation hΛ,i(t)≡h i(σΛ(t)).For the extremely diluted symmetric(SED)and the fully connected(FC) architectures the couplings are given by the Hebb ruleJ SED ij =c ijNA µ∈Pξµiξµj for i=j,J F C ii=0,(3)with the{c ij=0,1},i,j∈Λchosen to be i.i.d.r.v.with distribution Pr{c ij= x}=(1−C/N)δx,0+(C/N)δx,1and satisfying c ij=c ji.For the diluted symmetric model the architecture is a local Cayley-tree but, in contrast with the diluted asymmetric model,it is no longer directed such thatit causes a feedback from t≥2onwards.In the limit N→∞the probabilitythat the number of connections T i={j∈Λ|c ij=1}giving information to the site i∈Λ,is still a Poisson distribution with mean C=E[|T i|].Thereby it is assumed that C≪log N and in order to get an infinite average connectivityallowing to store infinitely many patterns one also takes the limit C→∞[10].At zero temperature all neurons are updated in parallel according to the rule σi(t+1)=g b(hΛ,i(t))g b(x)≡Qk=1s k[θ[b(s k+1+s k)−x]−θ[b(s k+s k−1)−x]](4)with s0≡−∞and s Q+1≡+∞.Here g b(·)is the gain function and b>0is the gain parameter of the system.Forfinite Q,this gain function is a step function. The gain parameter b controls the average slope of g b(·).3Localfield dynamicsIn order to measure the retrieval quality of the system one can use the Ham-ming distance between a stored pattern and the microscopic state of the networkd(ξµ,σΛ(t))≡1NA i∈Λξµiσi(t),µ∈P;aΛ(t)=1A ξ1i g b(h i(t)) ,a(t+1)P r= g2b(h i(t)) ,(7)where the convergence is in probability[11].In the above · denotes the av-erage both over the distribution of the embedded patterns{ξµi}and the initial configurations{σi(0)}.The average over the latter is hidden in an average over the localfield through the updating rule(4).Some remarks are in order.For the symmetric diluted model the sum over thesites i is restricted to T j,the part of the tree connected to neuron j.Moreover, for that model the thermodynamic limit contains the limit C→∞besides theN→∞limit.In this thermodynamic limit C,N→∞all averages have to be taken over the treelike structure,viz.1C i∈T j,and the capacity defined byα=p/N has to be replaced byα=p/C.In(7)the localfield is the main ingredient.Suppose that the initial con-figuration of the network{σi(0)},i∈Λ,is a collection of i.i.d.r.v.with mean E[σi(0)]=0,variance Var[σi(0)]=a0,and correlated with only one stored pat-tern,say thefirst one{ξ1i}:E[ξµiσj(0)]=δi,jδµ,1m10A(8) with m10>0.By the LLN one gets for the main overlap and the activity at t=0m1(0)≡lim(C),N→∞m1Λ(0)P r=1where the notation should be clear.In order to obtain the configuration at t=1 we have to calculate the localfield(1)at t=0.To do this we employ the probabilistic signal-to-noise ratio analysis([1]-[10]).Recalling the learning rule (3)we separate the part containing the signal from the part containing the noise. In the limit N→∞we then arrive ath i(0)≡limN→∞hΛ,i(0)D=ξ1i m1(0)+N(0,αa(0))(11)where the convergence is in distribution[11]and with N(0,V)representing a Gaussian random variable with mean0and variance V.We note that this struc-ture of the distribution of the localfield at time zero–signal plus Gaussian noise –is typical for all architectures treated in the literature.For a general time step t+1,a tedious study reveals that the distribution of the localfield is given by[9],[10]h i(t+1)=ξ1i m1(t+1)+N(0,αa(t+1))+χ(t)[F(h i(t)−ξ1i m1(t))+ασi(t)](12) where F=1for the fully connected architecture and F=0for the symmetrically diluted one.So,the localfield at time t consists out of a discrete part and a normally distributed part,viz.h i(t)=M i(t)+N(0,V(t))(13) where M i(t)and V(t)satisfy the recursion relationsM i(t+1)=χ(t)[F(M i(t)−ξ1i m1(t))+ασi(t)]+ξ1i m1(t+1)(14)V(t+1)=αa(t+1)A+Fχ2(t)V(t)+2FαAχ(t)Cov[˜rµ(t),rµ(t)].(15) The quantityχ(t)readsχ(t)=Q−1k=1f hµi(t)(b(s k+1+s k))(s k+1−s k)(16)where f hµi (t)is the probability density of hµi(t)in the thermodynamic limit.Fur-thermore,rµ(t)is defined asrµ(t)≡limN→∞1N i∈Λξµiσi(t),µ∈P\{1},(17)and˜rµ(t)is given by a similar expression withσi(t)replaced by g b(hΛ,i(t)−1 N ξµi rµΛ(t)).Finally,as can be read offfrom eq.(14)the quantity M i(t)consistsout of a signal term and a discrete noise term,viz.M i(t)=ξ1i m1(t)+αχ(t−1)σi(t−1)+F t−2t′=0α t−1 s=t′χ(s) σi(t′).(18)Since different architectures contain different correlations not all terms in these final equations are present,as is apparent through F.We remark that for the asymmetric diluted and the layered feedforward architecture M i(t)=ξ1i m1(t)so that in these cases the localfield consists out of a signal term plus Gaussian noise for all time steps[6],[7].For the architectures treated here we still have to determine the probabilitydensity f hi(t)in eq.(16).This can be done by looking at the form of M i(t)given byeq.(18).The evolution equation tells us thatσi(t′)can be replaced by g b(h i(t′−1)) such that the second and third terms of M i(t)are the sums of stepfunctions of correlated variables.These are also correlated through the dynamics with the normally distributed part of h i(t).Therefore,the localfield can be considered as a transformation of a set of correlated normally distributed variables x s,which we choose to normalize.Defining the correlation matrix W=(ρ(s,s′)≡E[x s x s′]) we arrive at the following expression for f hi(t)for the fully connected modelf hi(t)(y)= dx t t−2 s=0dx sδ y−M i(t)−2x W−1x T (19)with x={x s}=(x0,...x t−2,x t).For the symmetric diluted case this expression simplifies tof hi(t)(y)= [t/2] s=0dx t−2sδ y−ξ1i m1(t)−αχ(t−1)σi(t−1)−2x W−1x T (20)with x=({x s})=(x t−2[t/2],...x t−2,x t).The brackets[t/2]denote the integer part of t/2.4Gap structureThe equilibrium distribution of the local field can be obtained by eliminating the time dependence in the evolution equations (12)h i =ξ1im1+ηN(0,αa )+αχησi (21)with η=1/(1−χ)for the fully connected architecture and η=1for the extremely diluted one.The corresponding updating rule (4)σi =g b (˜h i +αχησi ),˜h i =ξ1i m 1i +ηN (0,αa )(22)in general admits more than one solution.A Maxwell construction (see,e.g.,refs.[9],[10],[12])can be made leading to a unique solutionσi =g ˜b (˜h i ),˜b =(b −αηχη√2αaη2× θ[˜b (s k +s k +1)+αχηs k −h ]−θ[˜b (s k +s k −1)+αχηs k −h ](25)meaning that (Q-1)gaps occur respectively at ˜b (s k +s k −1)+αχηs k −1<h <˜b (s k +s k +1)+αχηs k with width ∆h =2αχη/(Q −1).For analog networks no gaps occur.When ˜b ≤0the effective gain function (23)becomes two-state Ising-like as in the Hopfield model such that case only one gap occurs.For Q=2this expression simplifies tof(h)=12παaexp −(h−ξm−αχη)2η√2αaη2 θ(−h−αχη)(26)and for Q=3we havef(h)=12παaexp −(h−ξm−αχη)2η√2αaη2 θ(˜b2−h2)+12παaexp −(h−ξm+αχη)2Infigure4the gap boundaries in h as a function ofαare compared for retrieval and non-retrieval states in the symmetric diluted Q=3,b=0.2model. We remark that in this case the spin-glass states do not exist forα≤0.04[14] so that there is no gap for theseα-values.Forαlarge enough(α>0.465for retrieval states andα>0.252for spin-glass states)there exists one gap only since the effective gain function becomes Ising-like[14].More gaps with smaller widths are formed when increasing Q for both the fully connected and diluted models. For Q→∞the gaps disappear.Figure5compares the gaps for the spin-glass states in the fully connected and symmetric diluted Q=3models with b=0.5.Forα≤0.25there exist no spin-glass states in the diluted model[14]and forα≤0.004there are none in the fully connected model[13].When both do exist the gap widths are almost equal.So the dilution has some influence on the existence of the gap but,again, not on its width.Finally,fig.6presents the localfield distribution for the symmetric diluted Q=3,b=0.5model for a retrieval state(α=0.6,m0=0.7)just below the critical capacity.Only the distribution with pattern values+1is shown.It is asymmetric and two gaps are found at equilibrium.For pattern values0the distribution is symmetric and the gap locations and widths are the same(see eq.(25))but their height is different.In conclusion,we have studied the time evolution of the localfield in sym-metric Q-Ising neural networks both in the retrieval and spin-glass regime.We have found a gap structure in the localfield distribution depending on the spe-cific architecture and on the value of Q.The results agree with the numerical simulations we have performed.AcknowledgmentsThis work has been supported in part by the Fund of Scientific Research, Flanders-Belgium and the Korea Science and Engineering Foundation through the SRC program.The authors are indebted to A.Coolen,G.Jongen and V.Za-grebnov for constructive discussions.References[1]A.E.Patrick and V.A.Zagrebnov,Parallel dynamics for an extremely dilutedneural network,J.Phys.A:Math.Gen.23:L1323(1990);J.Phys.A:Math.Gen.25:1009(1992).[2]A.E.Patrick and V.A.Zagrebnov,On the parallel dynamics for the Little-Hopfieldmodel,J.Stat.Phys.63:59(1991).[3]T.L.H.Watkin and D.Sherrington,The parallel dynamics of a dilute symmetricneural network,J.Phys.A:Math.Gen.24:5427(1991).[4]A.E.Patrick and V.A.Zagrebnov,A probabilistic approach to parallel dynamicsfor the Little-Hopfield model,J.Phys.A:Math.Gen.24:3413(1991).[5]D.Boll´e,B.Vinck,and V.A.Zagrebnov,On the parallel dynamics of the Q-statePotts and Q-Ising neural networks,J.Stat.Phys.70:1099(1993).[6]D.Boll´e,G.M.Shim,B.Vinck,and V.A.Zagrebnov,Retrieval and chaos in ex-tremely diluted Q-Ising neural networks,J.Stat.Phys.74:565(1994).[7]D.Boll´e,G.M.Shim,and B.Vinck,Retrieval and chaos in layered Q-Ising neuralnetworks,J.Stat.Phys.74:583(1994).[8]D.Gandolfo,M.Sirugue-Collin and V.A.Zagrebnov,Local instability and oscilla-tions of trajectories in a diluted symmetric neural network,Network:Computation in Neural Systems9:563(1998)[9]D.Boll´e,G.Jongen and G.M.Shim,Parallel dynamics of fully connected Q-Isingneural networks,J.Stat.Phys.91:125(1998).[10]D.Boll´e,G.Jongen and G.M.Shim,Parallel dynamics of extremely diluted sym-metric Q-Ising neural networks,J.Stat.Phys.96:861(1999).[11]A.N.Shiryayev,Probability(Springer,New York,1984).[12]M.Shiino and T.Fukai,Self-consistent signal-to-noise analysis of the statisticalbehavior of analog neural networks and enhancement of the storage capacity,Phys.Rev.E48:867(1993).[13]D.Boll´e,H.Rieger and G.M.Shim,Thermodynamic properties of fully connectedQ-Ising neural networks,J.Phys.A:Math.Gen.27:3411(1994).[14]D.Boll´e,D.Carlucci and G.M.Shim,Thermodynamic properties of extremelydiluted Q-Ising neural networks,J.Phys.A:Math.Gen.33:6481(2000). [15]L.J.Schowalter and M.W.Klein,Analytic treatment of the hole in the internalfield distribution for an infinite-range spin glass,J.Phys.C:Solid State Physics12: L935(1979).10 [16]V.A.Zagrebnov and A.S.Chvyrov,The Little-Hopfield model:recurrence relationsfor retrieval-pattern errors,Sov.Phys.JETP68:153(1989)[17]A.C.C.Coolen and D.Sherrington,Order parameterflow in the fully connectedHopfield model near saturation,Phys.Rev.E49:1921(1994).h00.51f (h )Figure 1:A comparison of theoretical results and numerical simulations with N =6000for the local field distribution f (h )of a retrieval state in the Q =2system with network parameters α=0.13,m 0=0.5.Theoretical (simulation)results for time step t =0,1,2are indicated by a dotted curve (circles),a short-dashed curve (squares)and a long-dashed curve (diamonds).Simulations for t =10,20(stars,triangles)are shown and the full curve presents the equilibrium distribution.h00.250.5f (h )Figure 2:As in Fig.1,for a Q =2non-retrieval spin-glass state with the network parameters α=0.14,m 0=0.2.Further simulations for t =10(stars),t =30(crosses),t =50(filled circles)and t =100(filled squares)are shown.05101520Q00.511.5∆hFigure 3:The gap width ∆h for non-retrieval states as a function of Q for the gain parameter b =0.5for α=1(triangles),α=0.1(squares)and α=0.01(filled circles).The inset details the corresponding scaling properties.00.51α−1−0.500.51hFigure 4:The gap boundaries in h as a function of αfor retrieval (full curve)and non-retrieval (dashed curve)states for the Q =3symmetric diluted systems with gain parameter b =0.2.00.51 1.5α−1−0.500.51hFigure 5:The gap boundaries in h as a function of αfor spin-glass states in the fully connected (short-dashed curve)and symmetric diluted (long-dashed curve)Q =3system with gain parameter b =0.5.−2−10123h00.20.40.6f (h)Figure 6:The local field distribution f (h )of a retrieval state for pattern values +1in the symmetric diluted Q =3system with network parameters α=0.6,b =0.5,m 0=0.7.Results for t =0,1,2,∞are indicated by a dotted curve,a short-dashed curve,a long-dashed curve and a full curve respectively.。

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