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Nonlinear control of multibody systems with symmetries via shape change.

机译:通过形状改变对具有对称性的多体系统进行非线性控制。

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摘要

This dissertation makes contributions in three areas: local equilibrium controllability analysis for multibody systems controlled via shape change, motion planning for multibody systems via shape change, and control of specific multibody systems using shape change.; Equations of motion are formulated using the variational principle of Hamilton for two classes of multibody systems with symmetries: multibody systems with base body symmetry and multibody systems dependent on an advected parameter. Equilibrium manifolds and conserved quantities are investigated. Due to the presence of conserved quantities, the complete state of the multibody systems may not be controllable. Local configuration controllability and local equilibrium controllability are studied for these two classes of multibody systems. A general formula for symmetric products evolving on a configuration manifold suitable for multibody systems is derived. Important properties are obtained for symmetric products only involving shape control vector fields and for symmetric products involving a potential vector field dependent on an advected parameter. These properties reflect the multibody symmetries. The symmetric product properties are applied to controllability analysis. Simplified sufficient conditions for local configuration accessibility and local equilibrium controllability are obtained. Motion planning algorithms are developed for general mechanical systems based on a series expansion, using a regular perturbation technique. These algorithms are applied to rest-to-rest maneuvers for the two classes of multibody systems via shape change.; Three specific multibody control systems are studied. First, the Air Spindle Testbed controlled via two proof mass actuators is studied. Experiments are described that implement the motion planning approach. Experimental results demonstrate the effectiveness of the algorithms. Second, a free floating multibody spacecraft controlled via prismatic actuators is studied. Local fiber controllability analysis is carried out and global controllability properties are investigated. A motion planning algorithm is designed to achieve desired base body translational and rotational maneuvers. Third, the Triaxial Attitude Control Testbed controlled using shape change actuators is studied. Controllability conditions are obtained for several experimental setups; motion planning algorithms are constructed for rest-to-rest maneuvers.
机译:本文在三个方面做出了贡献:通过形状变化控制的多体系统的局部平衡可控性分析,通过形状变化的多体系统的运动计划以及使用形状变化的特定多体系统的控制。针对两类具有对称性的多体系统,使用汉密尔顿的变分原理来制定运动方程:具有基体对称性的多体系统和依赖于对流参数的多体系统。研究了平衡流形和守恒量。由于守恒量的存在,多体系统的完整状态可能无法控制。研究了这两类多体系统的局部构型可控性和局部平衡可控性。推导了在适用于多体系统的配置歧管上演化的对称产品的一般公式。对于仅涉及形状控制矢量场的对称积和涉及取决于对位参数的潜在矢量场的对称积,都获得了重要的性能。这些属性反映了多体对称性。对称的产品属性应用于可控性分析。获得简化的局部配置可及性和局部平衡可控性的充分条件。运动规划算法是使用常规扰动技术为基于系列扩展的通用机械系统开发的。这些算法通过形状改变被应用于两类多体系统的静态操纵。研究了三种特定的多体控制系统。首先,研究了通过两个质量执行器控制的空气主轴测试台。描述了实现运动计划方法的实验。实验结果证明了该算法的有效性。其次,研究了通过棱镜致动器控制的自由浮动多体航天器。进行了局部纤维可控性分析,并研究了整体可控性。设计运动计划算法以实现所需的基体平移和旋转操作。第三,研究了使用形状变化执行器控制的三轴姿态控制试验台。获得了几个实验设置的可控性条件;运动计划算法是为休息到休息的操纵而构造的。

著录项

  • 作者

    Shen, Jinglai.;

  • 作者单位

    University of Michigan.;

  • 授予单位 University of Michigan.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2002
  • 页码 202 p.
  • 总页数 202
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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