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Robust control of flexible structures: theory and experiments

机译:对柔性结构的鲁棒控制:理论和实验

摘要

NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in .pdf document.Stringent requirements envisioned for the pointing and shape accuracy of future space missions necessitate advances in the control of large flexible structures. These structures will be extremely flexible, with little natural damping and modes densely packed throughout the frequency domain. Due to their size and complexity, testing of these structures will lead to system models that are inaccurate for control purposes. Therefore, control design methods must be developed to account for model inaccuracies or uncertainties. Such methods should optimize the robustness and performance characteristics of control laws based on the accuracy of the design model.This thesis focuses on incorporating knowledge of the mismatch between the physical system and its mathematical models into the control design process. Control design models are developed to fit into the structured singular value [mu] framework that is used in the analysis and synthesis of control laws. To validate and verify theoretical developments, a flexible structure experiment is developed to investigate large flexible control problems in a laboratory environment. The Caltech experiment has a number of their attributes: closely spaced, lightly damped modes, collocated and noncollocated sensors and actuators combined with numerous modes in the controller crossover (roll off) region.The experimental structure is used to investigate several important issues related to control of flexible structures: tradeoffs between robustness and performance associated with uncertainty modeling for flexible structures, robust control of flexible modes in the controller crossover region and benefits and limitations of collocated versus noncollocated control design. A consistent trend in the results indicates that an accurate description of the flexible structure and model errors is required to synthesize high performance, robust control laws for flexible structures.
机译:注意:用[...]表示无法用纯ASCII呈现的文本或符号。 .pdf文件中包含摘要。未来太空飞行任务的指向性和形状精度要求严格,因此必须控制大型柔性结构。这些结构将非常灵活,几乎没有自然阻尼,并且在整个频域中密集地填充了模式。由于它们的大小和复杂性,对这些结构的测试将导致系统模型对于控制目的而言是不准确的。因此,必须开发控制设计方法以解决模型的不准确性或不确定性。这些方法应基于设计模型的准确性来优化控制律的鲁棒性和性能特征。本文着重于将物理系统及其数学模型之间的不匹配知识纳入控制设计过程。开发控制设计模型以适合用于控制律的分析和综合的结构化奇异值μ框架。为了验证和验证理论发展,开发了一种柔性结构实验,以研究实验室环境中的大型柔性控制问题。加州理工学院(Caltech)实验具有许多属性:紧密间隔,轻阻尼模式,并置和非并置传感器与执行器,以及在控制器分频(滚降)区域中的多种模式,该实验结构用于研究与控制相关的几个重要问题柔性结构:在与柔性结构的不确定性建模相关联的鲁棒性和性能之间进行权衡,在控制器交叉区域对柔性模式进行鲁棒控制以及并置与不并置控制设计的优点和局限性。结果的一致趋势表明,需要对柔性结构和模型误差进行准确的描述,才能为柔性结构合成高性能,鲁棒的控制律。

著录项

  • 作者

    Balas Gary John;

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  • 年度 1990
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