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Symbolic generation of equations of motion for dynamics/control simulation of large flexible multibody space systems.

机译:大型柔性多体空间系统动力学/控制仿真的运动方程符号生成。

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摘要

The formulation of equations of motion has become crucial in the successful design of very large and flexible space vehicles. This dissertation presents the derivation of explicit equations of motion for multibody flexible space systems via symbolic manipulation. This methodology generates very efficient computational algorithms in a reasonable amount of time and cost. Kane's dynamical equations are used to formulate the equations of motion. The procedure is considered optimal in the sense that it leaves with the analysts the tasks they are trained to perform, while transferring to the computer the manually prohibitive and distasteful algebraic manipulation and long derivation operations. The derivation allows the analysts to freely choose quantities such as the generalized speeds, the angular velocities, and the velocities, thus leading to a very flexible formulation.;The multibody system is idealized as a collection of interconnected bodies arranged in a topological tree configuration with the option that the bodies can form closed loops. The individual bodies in the system are either rigid or flexible. The flexible characteristics of the bodies are described by means of assumed admissible spatial functions. Bodies of the system are interconnected by hinges possessing zero to six degrees of relative motion freedom with unrestricted large rigid body motion. Linear or nonlinear springs and/or dampers can be incorporated for each degree of freedom at the hinge. Constraints in the multibody system are either holonomic or nonholonomic. Control systems and the external forces and torques acting on the multibody system are easily incorporated into the mathematical model. The explicit nonlinear differential equations of motion are casted in the form ;A general purpose program, named SYMBOD, written in a symbolic manipulation language is developed to generate the explicit equations of motion and is applied to two example problems.
机译:运动方程的公式化对于成功设计大型且灵活的太空飞行器至关重要。本文提出了通过符号操纵对多体柔性空间系统的显式运动方程的推导。该方法以合理的时间和成本生成了非常有效的计算算法。凯恩(Kane)的动力学方程式用于制定运动方程式。从让分析师留给他们训练的任务的意义上来说,该程序被认为是最佳的,同时将手动禁止且令人讨厌的代数运算和长时间推导操作传输到计算机。该推导使分析人员可以自由选择量,例如广义速度,角速度和速度,从而得出非常灵活的公式。多体系统被理想化为以拓扑树结构排列的互连体的集合,具有主体可以形成闭环的选项。系统中的各个主体是刚性的或柔性的。通过假定的允许空间功能来描述物体的柔韧性。系统的主体通过具有零到六度相对运动自由度的铰链相互连接,并具有不受限制的大刚体运动。线性或非线性弹簧和/或减震器可以在铰链处为每个自由度合并。多体系统的约束是完整的或非完整的。控制系统以及作用在多体系统上的外力和扭矩很容易合并到数学模型中。显式非线性运动微分方程的形式为;开发了用符号操作语言编写的通用程序SYMBOD,以生成显式运动方程,并将其应用于两个示例问题。

著录项

  • 作者

    Lee, Sheng Sam.;

  • 作者单位

    University of California, Los Angeles.;

  • 授予单位 University of California, Los Angeles.;
  • 学科 Aerospace engineering.
  • 学位 Ph.D.
  • 年度 1988
  • 页码 169 p.
  • 总页数 169
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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