A METHOD FOR SOLVING THE DYNAMICS OF MULTIBODY SYSTEMS WITH RHEONOMIC AND NONHOLONOMIC CONSTRAINTS

ＡＭＥＴＨＯＤＦＯＲＳＯＬＶＩＮＧＴＨＥＤＹＮＡＭＩＣＳＯＦＭＵＬＴＩＢＯＤＹＳＹＳＴＥＭＳＷＩＴＨＲＨＥＯＮＯＭＩＣＡＮＤＮＯＮＨＯＬＯＮＯＭＩＣＣＯＮＳＴＲＡＩＮＴＳ￥ＳｈｕｉＸｉａｏｐｉｎｇ（水小平）ＺｈａｎｇＹｏｎｇｆａ（张永发）（Ｄｅｐａｒ...     

ENERGY THEOREMS FOR SOLVING EQUATIONS OF DEFLECTIONS

In this paper the unit-dummy-load method is ge-neralized on the basis of Castigliano’s Theorem.Onthese grounds the general equations of deflection sur-faces of the structures.such as a kind of beams,platesand shells.are directly derived by the force method.We derived the equations of the deflection sur-faces of the rectangular thin plates and thick platesconsidering the effect of transverse shearing defor-mations with the inhomogeneous displacement boundaryconditions.At the same time we give the equations ofdeflection axes of the corresponding straight beams.The applications of the reciprocal theorem arealso generalized.Three simple calculated examples are given.     

THE RELATIONSHIP BETWEEN THE STABILITY AND THE OPTIMALITY OF LINEAR SYSTEMS(Ⅱ)

Different from the inverse problem put forward by R.E.Kalman, another kind ofinverse problem of linear optimal control is proposed and discussed in[1] as follows:Givenan asymptotically stable linear constant system and a nonnegative quadratic performanceindex, when can a state-feedback be separated from the stable system so that this state-feedback control law is optimal for the given index? In this paper this problem is extended.Similar conclusions are obtained for linear discrete systems and linear time-variablesystems. According to these conclusions we can say that the correspondence between theasymptotically stable system and the optimal feedback system is the inherent character ofall kinds of linear systems.     

IMPULSIVE CONTROL FOR THE STABILIZATION AND SYNCHRONIZATION OF LUR'E SYSTEMS

IntroductionInpractice ,thereexistmanyexamplesofimpulsivecontrolsystems (seeRefs.[1 ,2 ,3 ] ) .Recently ,impulsivecontrolhasbeenwidelyusedtostabilizeandsynchronizechaoticsystems(seeRefs.[4～ 1 5] ) .Forexample,thepredictivePoincarecontrol[4 ]andtheoccasionalproportionalfeedbackcontrol[5 ]aretwoimpulsivecontrolschemeswithvaryingimpulsiveintervals.Yangetal.inRefs.[7,1 1 ]studied ,respectively ,thestabilizationandsynchronizationofaclassofchaoticsystemscalledLorenzsystems .YangandChuainRef.[1 …     

THE ANALYTIC RESOLUTIONS AND APPLICATIONS OF THE NON－LINEAR SEEPAGE FLOW EQUATIONS OF COAL INFUSION

ＴＨＥＡＮＡＬＹＴＩＣＲＥＳＯＬＵＴＩＯＮＳＡＮＤＡＰＰＬＩＣＡＴＩＯＮＳＯＦＴＨＥＮＯＮ－ＬＩＮＥＡＲＳＥＥＰＡＧＥＦＬＯＷＥＱＵＡＴＩＯＮＳＯＦＣＯＡＬＩＮＦＵＳＩＯＮＺｈａｎｇＹａｎｓｏｎｇ（张延松）（ＲｅｃｅｉｖｅｄＪａｎ．１,１９９４．Ｃｏ...     

THE PERTURBATION FINITE ELEMENT METHOD FOR SOLVING THE PLANE PROBLEM IN CONSIDERATION OF LINEAR CREEP

In this paper, amethod (PFMC) for solving plane problem of linear creep is presented by using perturbation finite element. It can be used in plane problem in consideration of creep, such as reinforced concrete beam, prestressed concrete beam, reinforced concrete cylinder and reinforced concrete tunnel in elastic or visco-elastic medium, as well as underground building and so on. In the presented method, the assumption made in the general increment method that variables remain constant in a divtded time interval is not taken. The accuracy is improved and the length of time step becomes larger. The computer storage can be reduced and the calculating efficiency can be increased. Perturbation finite element formulae for four-node quadrilateral isoparametric element including reinforcement are established and five numerical examples are given. As contrasted with the analytical solution, the accuracy is satisfactory.     

APPLICATION 0F THE THEORY OF BRANCHING OF SOLUTIONS OF NONLINEAR EQUATIONS IN THE ESTIMATION OF POLE PERTURBANCE OF LINEAR CLOSED-LOOP SYSTEMS

When the state and input matrices of a multivariable lineartime-invariant system are perturbed.the problem of the es-timation of pole perturbance of closed-loop system is con-sidered by making use of the theory of branching of solutionsfor nonlinear equations.     

THE THEOREM OF THE STABILITY OF LINEAR NONAUTONOMOUS SYSTEMS UNDER THE FREQUENTLY-ACTING PERTURBATION

In the paper a theorem on the stability of linear nonautonomous system under thefrequently-acting perturbation has been given and proved on the basis of Malkin＇sTheorem.     

CRITERIA FOR THE EXISTENCE OF SOLUTIONS TO RANDOM INTEGRAL AND DIFFERENTIAL EQUATIONS

In[1],we proved a general random fixed point theorem and gave some applications.Inthis paper,we shall give further applications of the theorem.We first obtain a randomDarbo’s fixed point theorem,using the theorem,we give the criteria for the existence ofsolutions under compactness hypotheses to nonlinear random volterra integral equationsand the Cauchy problem of nonlinear random differential equations.Our theorems improveand generalize some main results of Lakshmikanthem,Vaughn as well as De Blasiand Myjak.     

IMPULSIVE CONTROL FOR THE STABILIZATION AND SYNCHRONIZATION OF LUR＇ E SYSTEMS

An impulsive control scheme of the Lur‘e system and several theorems on stability of impulsive control systems was presented, these theorems were then used to find the conditions under which the Lur‘e system can be stabilized by using impulsive control with varying impulsive intervals. The parameters of Lur‘e system and impulsive control law are given, a theory of impulsive synchronization of two Lur‘e system is also presented. A numerical example is used to verify the theoretical result.     

旋转薄圆盘的行波动力学特性分析

旋转圆盘是广泛应用于旋转机械装置中的基本结构元件,圆盘在高速旋转状态下会表现出与低速或非旋转状态下迥异的力学性能.本文对高速旋转薄圆盘横向振动的行波动力学特性进行了分析,建立了考虑离心力引起的薄膜内力影响下的动力学控制方程以及相应的边界条件.采用伽辽金法数值模拟了旋转圆盘前、后行波振动频率和动力屈曲失稳临界转速随着圆盘几何参数如半径比、厚度的变化规律,以及材料参数对于振动频率和临界转速的影响等.本文的数值计算可以同时给出圆盘旋转的前、后行波频率,并且结果与实验结果吻合良好.     

计算结构力学在桥梁结构施工设计与施工控制中的应用

随着大跨径桥梁结构在工程中应用日趋广泛,其施工控制问题也越来越受到工程界的重视。本文将计算结构力学方法引入桥梁结构的施工设计与控制,给出桥梁结构竣工后受力状态、施工各阶段理想状态的确定、施工控制方法及其程序系统的设计思想。     

Computations of a laminar backward‐facing step flow at Re=800 with a spectral domain decomposition method

The two‐dimensional laminar incompressible flow over a backward‐facing step is computed using a spectral domain decomposition approach. A minimum number of subdomains (two) is used; high resolution being achieved by increasing the order of the basis Chebyshev polynomial. Results for the case of a Reynolds number of 800 are presented and compared in detail with benchmark computations. Stable accurate steady flow solutions were obtained using substantially fewer nodes than in previously reported simulations. In addition, the problem of outflow boundary conditions was examined on a shortened domain. Because of their more global nature, spectral methods are particularly sensitive to imposed boundary conditions, which may be exploited in examining the effect of artificial (non‐physical) outflow boundary conditions. Two widely used set of conditions were tested: pseudo stress‐free conditions and zero normal gradient conditions. Contrary to previous results using the finite volume approach, the latter is found to yield a qualitatively erroneous yet stable flow‐field. Copyright © 1999 John Wiley & Sons, Ltd.     

An Alternative Stability Analysis Technique for the Simplest Walker

We revisit the simplest walker studiedearlier by Garcia and co-workers. We extend the small-slope stability analysis to second order, substantially improving accuracy, andalso provide some details left out of the earlier work.We develop an alternative (reverse) approach for the stabilityanalysis, which involves shorter calculations: for stability analysis upto any given order, the new procedure requires calculations to one order less than the previous (forward) procedure. The stabilityresults obtained by the two methods are, nevertheless, equivalent.     

Numerical study on the vortex motion patterns around a rotating circular cylinder and their critical characters

A hybrid finite difference and vortex method (HFDV), based on the domain decomposition method (DDM), is used for calculating the flow around a rotating circular cylinder at Reynolds number Re=1000, 200 and the angular‐to‐rectilinear speed ratio α∈(0.5, 3.25) respectively. A fully implicit third‐order eccentric finite difference scheme is adopted in the finite difference method, and the deduced large broad band sparse matrix equations are solved by a highly efficient modified incomplete LU decomposition conjugate gradient method (MILU‐CG). The long‐time, fully developed features about the variations of the vortex patterns in the wake, as well as the drag and lift forces on the cylinder, are given. The calculated streamline contours are in good agreement with the experimentally visualized flow pictures. The existence of the critical state is confirmed again, and the single side shed vortex pattern at the critical state is shown for the first time. Also, the optimized lift‐to‐drag force ratio is obtained near the critical state. Copyright © 1999 John Wiley & Sons, Ltd.     

绕旋转圆柱流动涡尾流结构和临界状态特性

采用作者提出的基于区域分解、有限差分法与涡法杂交的数值方法,结合高阶隐式差分格式,和以修正的不完全ＬＵ分解为预处理器的共轭梯度法作求解器．系统地研究了雷诺数Ｒｅ＝１０００,旋转速度比ａ∈（０．５,３．２５）范围内,绕旋转圆柱从突然起动到充分发展,长时间内尾流旋涡结构和阻力、升力系数的变化规律．计算所得流动图案与实验流场显示符合很好．数值试验证实了临界状态的存在,并首次给出了临界状态时的旋涡结构特性,指出最佳升阻比也在该状态附近得到     

一种基于多尺度和改进支持向量机的光纤陀螺温度漂移建模与补偿方法

为了提升光纤陀螺温度漂移模型建模的准确性及补偿的效果,提出了一种基于改进支持向量机的多尺度建模和回归方法。首先分析了造成光纤陀螺温度漂移的关键因素,给出了建模的属性参数和温度试验。然后根据经验模态分解得到的本征模态函数排列熵的变化趋势,得出了回归精度和熵之间的变化关系,进而提出了基于信号分解的多尺度回归方法。为了提高上述多尺度回归算法的适应性,在传统支持向量机的基础上,提出了基于组合核函数的支持向量机回归算法,以适应不同特性的回归数据集。为了进一步提高回归精度,基于降低回归数据复杂度的分段回归思想,在上述多尺度回归的基础上提出了双-多尺度回归,并验证了方法的有效性。最后,将提出的算法以实际的光纤陀螺温度漂移数据进行验证,结果表明,相比于传统的支持向量机和反向传播神经网络具有更好的回归精度,温度漂移模型也更加精确,以均方误差指标为例,回归精度提升了两个数量级。