树形带球铰的多刚体系统动力学方程的建立方法

本文提出了一种建立树形带球铰多刚体系统动力学方程的新方法,运用约束系统动力学研究成果,提出了广义刚体的概念以代替多刚体系统的子系统,并借助于广义刚体的不断扩充,求得了多刚体系统动力学方程建立的递推方法,该方法简单直观,几何概念清楚,并允许多刚体系统的扩充,且便于进行计算机符号处理。     

变结构多刚体系统的动力学问题

本文深入地研究了多刚体系统结构变化的动力学问题,建立下相应的数学模型,讨论了有关的数字仿真,并给出了一个算例,结果是满意的,对所论课题,本文工作同以往相比更准确完整,更便于计算机编程。     

刚体动力学的拟变分原理及其应用

为了适应航天事业发展的需要,极有必要开展多柔体系统的理论分析.作为应用非保守系统的拟变分原理进行多柔体动力学的理论分析的组成部分,研究了刚体动力学的拟变分原理及其应用:建立了刚体动力学的拟变分原理,推导出刚体动力学的拟变分原理的拟驻值条件; 建立了刚体动力学的广义拟变分原理,说明了应用广义拟变分原理求得问题的解析解和数值解的途径; 最后,借助算例说明了应用变分方法来研究刚体动力学问题的优越性.      

刚体动力学的速度空间中的变分原理

本文将[1]给出的质点系的速度空间中的变分原理用于刚体,得出刚体动力学的速度空间中的变分原理。     

多刚体系统动力学微机通用软件DASRB—数学模型与结构

为适应国内微机拥有较普遍的现状,在微机上运行的多刚体系统动力学分析通用软件DASRB已被开发使用。本文介绍了该软件的数学模型及软件特性。文末给出该软件讨论卫星太阳帆板展开的算例。     

多刚体系统分离策略及释放动力学研究

紧密连接的多刚体系统可在脱离运载航天器后在轨自主分离,无需多次利用航天器发射装置或在航天器中安装多个发射装置进行分离释放,从而有效提高运载航天器空间利用率, 简化分离释放操作和降低碰撞风险.本文针对多刚体系统的在轨分离释放问题, 研究在轨分离策略及释放过程动力学.首先, 考虑刚体相对运动及姿态变化,基于虚功原理及自然坐标方法建立单个刚体的动力学模型.考虑多刚体系统在轨分离释放阶段的轨道运动和连接约束变化,计入分离时刚体间的相互作用,利用拉格朗日乘子法获得含连接约束的非线性动力学模型. 考虑到实际工程应用,在多刚体系统分离释放阶段,通过安装在刚体间每个接触表面4个角上的弹射装置实现自主分离. 其次,为保证分离过程中刚体之间无碰撞发生, 规划了多刚体系统的分离时序,并基于不同弹射方向及分离顺序设计了两种分离释放方案. 最后,通过算例研究分析了在轨分离释放过程中刚体的非线性动力学行为,验证了分离释放方案的有效性.      

刚体单元及其在多体系统动力学中的应用

多体系统动力学分析软件要求人工输入形状复杂物体的质量、质心位置和转动惯量,而实际上这些参量并不容易获得。本文探索了一种以组成物体的刚体单元为基本要素的新方法,并结合实际需要具体构造了刚性四面体和刚性梁单元。以刚体单元为基础并内嵌网格剖分模块的分析软件能够自动获得这些参数,从而具备处理任何复杂系统的能力。仿真结果的对比分...     

多刚体系统动力学的正则方程及数值解法

本文研究了多刚体系统动力学的正则方程,并由此论证了多刚体系统动力学方程的运动稳定性态.在比较不同数值积分方法的基础上,得出结论:基于正则方程的数值积分方法能较好地保证计算精度.     

关于刚体系统碰撞问题的动力学普遍定理解法

关于刚体系统碰撞问题的动力学普遍定理解法黎邦隆，黎之奇（湖南大学，长沙４１００８２）（中科院力学所，北京１０００８０）对较复杂的刚体系统的碰撞问题，一般都用冲力情况下的拉格朗日方程解答．因为通常都认为，用动力学普遍定理，就要将系统拆开，于是导致各刚体...     

燃料消耗下充液航天器等效动力学建模与分析

在轨航天器贮腔内的液体可能表现出多种不同的运动模式, 主要包括液体相对于贮腔的整体性刚体运动、自由液面横向晃动、液体起旋后逐步发生明显的旋转晃动及液体自旋运动; 复合三自由度刚体摆晃动模型能够较为全面地描述这些液体运动模式, 同时为研究起旋阶段的液体晃动动力学问题提供了有效手段. 本文对非线性液体晃动刚体摆复合模型作进一步发展, 考虑模型等效参数随贮腔充液比的变化, 提出了变参数的刚体摆复合模型, 该模型适用于研究燃料消耗下非线性晃动类充液航天器大范围运动耦合动力学问题. 采用刚体摆复合模型对球形贮腔内的液体晃动进行等效后, 基于混合坐标意义下的拉格朗日方程推导了一类充液航天器轨道-姿态-晃动全耦合的动力学方程组, 并展开了充液航天器大角度三轴稳定姿态机动和零冲量轨道机动仿真以及航天器耦合动力学响应特性分析. 研究表明: 液体相对于贮腔的运动会造成航天器主刚体位置发生偏移, 当航天器在执行零冲量机动时, 燃料消耗会造成航天器的轨道平动速度无法收敛到零; 贮腔偏心布放时, 航天器在执行轨道机动过程中贮腔内液体易发生剧烈而且形式复杂的晃动行为, 进而可能造成航天器刚体运动的不稳定.      

动态设计变量优化方法及其在工程静力学通用程序设计中的应用

本文提出动态设计变量优化新方法并解决理论和工程问题，该方法首先构建目标函数框架，然后根据具体问题的输入条件，动态地进行设计变量分配和合理排序，形成实际问题的动态目标函数。基于动态设计变量优化方法，编制出一个能解决单刚体、刚体系的平面和空间问题、摩擦问题和桁架所有工程静力学平衡问题的通用程序，并通过实例分析验证。为解决更多工程领域问题提供有效新观点。     

含刚性体可展开结构的展开过程动力学分析方法

在可展结构中设置刚性体可以有效提高展开效率,保证形状精度,因此含刚性体可展结构具有较高的实用价值。刚性体按需要可为刚性曲板等,一般形状复杂且形式多样,含任意形状刚性体可展结构的展开过程动力学分析比较困难。本文以笛卡尔坐标系下节点坐标及位移为变量,利用广义逆矩阵建立了一种通用的刚性体动力学方程,给出了利用Newmark—...     

The influence of variable stiffness of teeth on dynamic loads in single-gear transmission

Summary In this paper, the influence of the variable stiffness of mating gear teeth on dynamic loads occurring between teeth in a single-gear transmission is investigated using a discrete-continuous model consisting of two torsionally deformable ponderable shafts and four rigid bodies. The stiffness is described by a harmonic function of time. Considerations by means of the wave method enable to determine dynamic loads in steady as well as in transient states. Numerical calculations are concentrated on the determination of the amplitudes of dynamic loads on gear teeth with respect to revolution per minute. Received 4 March 1997; accepted for publication 12 September 1997     

考虑刚弹耦合作用的柔性多体连续系统动力学建模

基于Ｈａｍｉｌｔｏｎ原理建立起一般柔性体连续系统的动力学建模方法,进而以水平面内作大范围回转运动的柔性梁为例,在Ｅｕｌｅｒ－Ｂｅｒｎｏｕｌｌｉ梁模型的假设前提下,根据轴向不可伸长的柔性梁的几何约束条件;推导出作大范围刚体运动的柔性梁连续系统的一致线性化振动微分方程．采用假设模态法对其离散化,导出考虑刚弹耦合作用的柔性梁有限维离散化动力学模型．最后给出仿真算例,验证了该方法的有效性．     

Melnikov's method for rigid bodies subject to small perturbation torques

Summary In this paper, the global motion of rigid bodies subjected to small perturbation torques, either conservative or dissipative, is investigated by means of Melnikov's method. Deprit's variables are introduced to transform the equations of motion into a standard form which is rendered suitable for the application of Melnikov's method. The Melnikov method is used to predict the transversal intersections of stable and unstable manifolds for the pertubed rigid-body motion. The chosen examples are a self-excited rigid body subject to a small periodic torque in a viscous medium, and the heavy rigid body. It is shown in both cases that there exist transversal intersections of heteroclinic orbits for certain ranges of parameter values.     

Application of the integral manifold method to the analysis of the spatial motion of a rigid body fixed to a cable

We analyze the spatial motion of a rigid body fixed to a cable about its center of mass when the orbital cable system is unrolling. The analysis is based on the integral manifold method, which permits separating the rigid body motion into the slow and fast components. The motion of the rigid body is studied in the case of slow variations in the cable tension force and under the action of various disturbances.We estimate the influence of the static and dynamic asymmetry of the rigid body on its spatial motion about the cable fixation point. An example of the analysis of the rigid body motion when the orbital cable system is unrolling is given for a special program of variations in the cable tension force. The conditions of applicability of the integral manifold method are analyzed.     

Analysis of a rigid body obliquely impacting granular matter

The model of the oblique rigid body impact with a granular matter is studied. The force acting on the body is a linear superposition of a static (velocity-independent) friction force and a dynamic (velocity-dependent) resistance force. The impact of a sphere, a mathematical and a compound pendulum are modeled and simulated using different initial impact velocity conditions and different impact angles. We analyze how rapidly the rigid body impacting a granular media slows upon collision. For most of the analyzed cases the rigid body under high-force impact (higher initial velocity) comes to rest faster in a granular matter than the same body under low-force impacts (lower initial velocity). Researchers were able to explain this interesting phenomena, not shared by solids or liquids, for the vertical impact of spheres. The simulations for some configurations with small initial impact angles show that as the speed at which the rigid body impacts the media increases, the later it will come to rest.

     

Synthesis of a controller for stabilizing the motion of a rigid body about a fixed point

A method for the approximate design of an optimal controller for stabilizing the motion of a rigid body about a fixed point is considered. It is assumed that rigid body motion is nearly the motion in the classical Lagrange case. The method is based on the common use of the Bellman dynamic programming principle and the averagingmethod. The latter is used to solve theHamilton–Jacobi–Bellman equation approximately, which permits synthesizing the controller. The proposed method for controller design can be used in many problems close to the problem of motion of the Lagrange top (the motion of a rigid body in the atmosphere, the motion of a rigid body fastened to a cable in deployment of the orbital cable system, etc.).     

Rigid body coupled rotation around no intersecting axes

In this paper rigid body dynamic with coupled rotation around axes that are not intersecting is described by vectors connected to the pole and the axis. These mass moment vectors are defined by K. Hedrih. Dynamic equilibrium of rigid body dynamics with coupled rotations is described by vector equations. Also, they are used for obtaining differential equations to the rotor dynamics. In the case where one component of rotation is programmed by constant angular velocity, the non-linear differential equation of the system dynamics in the gravitational field is obtained and so is the corresponding equation of the phase trajectory. Series of phase trajectory transformations in relation with changes of some parameters of rigid body are presented.