基于小变形的柔性多体系统动力学建模方法研究

引入非线性变形场描述,建立了基于小变形的柔多体系统动力学模型,解决了传统动力学建模方法存在的对变形广义坐标过早线性化的缺陷。对旋转梁式构件进行了动力学仿真,仿真结果表明传统方法不适合用于高速旋转的柔性体动力学建模,本文提出的动力学模方法为解决实际工程中各种复杂结构动力学分析提供了有力工具。     

含动力刚化项的一般多柔体系统动力学研究

为获取柔性体的动力刚化项,将任意形状柔性体的非线性变形场表达为直至广义坐标的二阶小量形式．在小变形条件下,用Green应变张量得到了柔性体的耦合形函数．把约束引入多柔体系统,依据Kane方程建立了包含动力刚化项的一般柔性多体系统动力学方程．通过数值仿真算例,界定了传统多柔体系统动力学建模方法的适用范围．     

多柔体系统刚柔耦合动力学有限单元法

传统的多柔体系统动力学建模理论,往往基于小变形线性动力学的基本假定,采用线性的Cauchy应变理论描述应变—位移关系。但是,对于具有刚性旋转的位移场来说,Cauchy应变理论并不适用。本文采用Green-Lagrange应变理论,描述有大位移运动的梁单元的非线性位移—应变关系,通过对应变能的分析和线性化处理,建立起相对变形坐标一阶精确的一致线性化的多柔体系统有限元模型,仿真算例的结果验证了该方法的有效性和结构中的几何非线性对系统动力学响应的重要作用。     

多柔体系统刚柔耦合动力学有限单元法

传统的多柔体系统动力学建模理论 ,往往基于小变形线性动力学的基本假定 ,采用线性的Cauchy应变理论描述应变—位移关系。但是 ,对于具有刚性旋转的位移场来说 ,Cauchy应变理论并不适用。本文采用Green Lagrange应变理论 ,描述有大位移运动的梁单元的非线性位移—应变关系 ,通过对应变能的分析和线性化处理 ,建立起相对变形坐标一阶精确的一致线性化的多柔体系统有限元模型 ,仿真算例的结果验证了该方法的有效性和结构中的几何非线性对系统动力学响应的重要作用。     

多柔体系刚以了条耦合动力学有限单元法

传统的多柔体系统动力学建模理论,往往基于小变形线性动力学的基本假定,采用线性的Cauchy应变理论描述应变一位移关系。但是,对于具有刚性旋转的移场来说,Cauchy应变理论并不适用。本文采用Green-Lagrange应变理论,描述有大位移运动的梁单元的非线性位移－应变关系,通过对应变能的分析和性线化处理,建立起相对变形坐标一阶精确的一致线性化的多柔体分析系统有限元模型,仿真算例的结果验证了该方法的有效性和结构中的几何非线性对系统动力学响应的重要作用。     

柔性多体系统动力学——有限段方法

采用有限段方法建立柔性梁式的离散模型，基于Ｋａｎｅ方程的Ｈｕｓｔｏｎ方法建立柔性多体系统学方法，该方程计入了梁式构件的几何非线性变形的惯性影响，在求解过程中，引入了相对位移的模态变换以提高计算效率，通过典型实验验证了有限段方法可解决具有几何非线性变形的柔性梁式构件的多体系统的动力学问题。     

柔性体动力学建模中的过早线性化问题

论述了采用传统动力学建模方法建立空间飞行器柔性附件动力学方程时过早线性化问题,揭示了这种方法建立的动力学方程的缺陷,即失去了一些重的刚柔耦合项,本文采用Ｋａｎｅ方法建立动力学方程的一般公式,并确定了采用传统动力学方法建立动力学方程所失去的项,进一步探讨了工于构件小变形的空间飞行器柔性附件动力学的建模方法。     

具有有限弹性变形部件的多体系统动力分析

本文主要论述了具有有限弹性变形部件的多体系统非线性动力学控制方程。方程中包含几何非线性和惯性非线性两方面的因素。几何非线性是考虑了应变-位移关系式中的二次项,在采用计及剪切和截面回转惯性的Timoshenko梁单元的情况下得到一个新的几何非线性刚度阵,而惯性非线性则是考虑了部件大幅度的转动。文中采用欧拉参数来描述部件参考系的转动。三个数值例子是用来考察上述因素在系统瞬态响应中的影响。     

柔性多体系统动力学的研究进展与建模方法

随着空间技术和空间应用等领域需求的不断扩大以及机器人技术的发展,使得考虑部件柔性的系统动力学分析的研究备受重视。简述了柔性多体系统动力学的研究进展,讨论了柔性多体系统动力学建模过程中的建模方法、离散化方法以及坐标系的选择,最后总结并展望了柔性多体系统动力学后续要研究的问题。     

柔性多体机械系统动力学递推方程

基于Ｊｏｒｄａｉｎ变分原理建立含闭环的复杂柔性多体机械系统递推形式动力学通用方程．用图论描述系统的拓外结构，分别用铰相对坐标与模态坐标描述相邻物体间的大位移运动及物体的弹性变形．对含闭环的系统，用铰切割方法建立相应的运动学约束方程，结果为一组拆合形式的动力学递推方程和折合形式的加速度约束方程，适合于建立该类系统的并行计算方法和用于实时动力学仿真。     

多柔体系统动力学建模程序源代码的软件实现

采用将较长表达式分割并用变量替换的递归循环方法,编制了相应的符号处理程序模块,将由Mathematica得到的公式化简并转化成FORTRAN格式的源代码．通过算例说明该程序是正确、有效且可靠的．     

柔性空间飞行器姿态动力学响应仿真的研究

将带有弹性附件的柔性空间飞行器模化为多体簇系统，考虑相邻体间相对运动为缓慢的实际特点，在忽略高阶非线性项的情况下，利用Ｄ’Ａｌｅｍｂｅｒｔ虚功原理，采用混合坐标的方法，建立了该多体簇系统的基本动力学方程。其中表示弹性附件的弹性变形的模态是约束模态，以上术方程为基础，采用状态空间求解方法，偏制了相应的动力学响应仿真程序；文章最后给出了仿真算例。     

Dynamic modeling and simulation for the flexible spacecraft with dynamic stiffening

A rigid flexible coupling physical model which can represent a flexible spacecraft is investigated in this paper. By applying the mechanics theory in a non-inertial coordinate system, the rigid flexible coupling dynamic model with dynamic stiffening is established via the subsystem modeling framework. It is clearly elucidated for the first time that, dynamic stiffening is produced by the coupling effect of the centrifugal inertial load distributed on the beam and the transverse vibration deformation of the beam. The modeling approach in this paper successfully avoids problems which are caused by other popular modeling methods nowadays: the derivation process is too complex by using only one dynamic principle; a clearly theoretical explanation for dynamic stiffening can't be provided. First, the continuous dynamic models of the flexible beam and the central rigid body are established via structural dynamics and angular momentum theory respectively. Then, based on the conclusions of orthogonalization about the normal constrained modes, the finite dimensional dynamic model suitable for controller design is obtained. The numerical simulation validations show that: dynamic stiffening is successfully incorporated into the dynamic characteristics of the first-order model established in this paper, which can indicate the dynamic responses of the rigid flexible coupling system with large overall motion accurately, and has a clear modeling mechanism, concise expressions and a good convergence.     

Complete geometric nonlinear formulation for rigid-flexible coupling dynamics

A complete geometric nonlinear formulation for rigid-flexible coupling dynamics of a flexible beam undergoing large overall motion was proposed based on virtual work principle, in which all the high-order terms related to coupling deformation were included in dynamic equations. Simulation examples of the flexible beam with prescribed rotation and free rotation were investigated. Numerical results show that the use of the first-order approximation coupling (FOAC) model may lead to a significant error when the flexible beam experiences large deformation or large deformation velocity. However, the correct solutions can always be obtained by using the present complete model. The difference in essence between this model and the FOAC model is revealed. These coupling high-order terms, which are ignored in FOAC model, have a remarkable effect on the dynamic behavior of the flexible body. Therefore, these terms should be included for the rigid-flexible dynamic modeling and analysis of flexible body undergoing motions with high speed. Foundation item: Project(10772113) supported by the National Natural Science Foundation of China     

数控凸轮轴磨床运动误差分析与建模技术

为了对某数控凸轮轴磨床的运动误差进行分析和建模,分析研究了各运动部件间运动形式和误差类型,运用相邻体坐标系间的运动变化来表达2相邻体之间的运动情况,建立了相邻体之间的理想运动方程和有误差情况下的实际运动方程.将相邻体间的实际运动方程进一步推广到任意低序体阵列分析当中,为研究多分支数控凸轮轴磨床误差建模提供理论基础.将复杂的多分支链数控凸轮轴磨床抽象为简单的多体系统,对各运动部件建立相应的体坐标系和运动参考坐标系,求出相邻体间对应的变换矩阵.最后,将机床运动部件划分为"工件-床身"和"砂轮-床身"2条运动链,提出了有误差影响情况下实现精密加工约束条件方程为P_w=P_t,且对该方程进行了求解,为数控凸轮轴磨床误差补偿的研究提供了必要条件.结果表明:误差补偿后的机床加工精度显著提高.     

Dynamic modeling and simulation for the rigid flexible coupling system with a non-tip mass

The rigid flexible coupling system with a mass at non-tip position of the flexible beam is studied in this paper. Using the theory about mechanics problems in a non-inertial coordinate system, the dynamic equations of the rigid flexible coupling system with dynamic stiffening are established. It is clearly elucidated for the first time that, dynamic stiffening is produced by the coupling effect of the centrifugal inertial load distributed on the beam and the transverse vibration deformation of the beam. The modeling approach in this paper successfully solves problems of popular modeling methods nowadays: the derivation process is too complex by using only one dynamic principle; a clearly theoretical mechanism for dynamic stiffening can't be offered. First, the mass at non-tip position is incorporated into the continuous dynamic equations of the system by use of the Dirac function and the Heaviside function. Then, based on the conclusions of orthogonalization about the normal constrained modes, the finite dimensional state space equations suitable for controller design are obtained. The numerical simulation results show that: dynamic stiffening is included in the first-order model established in this paper, which indicates the dynamic responses of the rigid flexible coupling system with large overall motion accurately. The results also show that the mass has a softening effect on the dynamic behavior of the flexible beam, and the effect would be more obvious when the mass has a larger mass, or lies closer to the tip of the beam.     

The bond graph model of planar flexible multibody mechanical systems and its dynamic principle

Toincreasethereliabilityandefficiencyofthedy namicanalysisofflexiblemultibodysystems,differentprocedureshavebeenproposedinpreviousworks[1,2].Buttheseproceduresareonlysuitableforasingleener gydomain,suchasastrictmechanicalone,andcan notdealwiththeproblemsofcomputeraideddynamicanalysisofplanarflexiblemultibodymechanicalsys temscontainingthecouplingofmulti energydomains.Bondgraphs[3]havepotentialapplicationsinanalyzingsuchcomplexsystemsbecauseoftheirabilitytode scribethedynamicsofinteractingsyste…     

动力刚化系统动力学建模方法的研究

具有大范围、高速运动的柔性体，即使在小变形范围内，运动和变形的耦合将产生动力刚化现象，本文提出一种研究动力刚化系统新的方法，建立了求解动力刚化系统逆问题的数学模型，拓宽了动力刚化问题的研究范围，该项研究对以柔性体为代表的航天器中的构件、机器人和高速机构等机械诉设计、动力学仿真和减振控制，具有重要意义。