Influence of complexity relaxation and convex hull manipulation on LMI based control design

Alexandra Szöllosi, P. Baranyi
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引用次数: 7

Abstract

The paper investigates how the complexity and the convex hull determined by the vertexes of the TP model representation of a given quasi Linear Parameter Varying state-space model influence the stable parameter region achievable via Linear Matrix Inequality based control design. The paper applies the Relaxed TP model transformation based Control Design Framework that supports both the complexity-accuracy trade-off of the TP model representation and convex hull manipulation separately executable on all components of the control system to be derived. Some specialization and further relaxation of the framework is also proposed here for frequent cases when all components of the system is handled in TP model form. The framework is also extended with a TP model interpolation technique to perform a systematic convex hull manipulation. The overall investigation is done on the complex NATA model of the three degree of freedom aeroelastic wing section model including Stribeck friction. The paper concludes and via the example proofs that both the complexity and the convex hull strongly influences the feasibility of the design. Further the paper proofs that the separate convex hull manipulation of the given model done for controller and the observer design also has to be taken into consideration.
复杂性松弛和凸包操作对基于LMI的控制设计的影响
本文研究了给定准线性参数变状态空间模型的TP模型表示的顶点的复杂性和凸壳如何影响基于线性矩阵不等式的控制设计可实现的稳定参数区域。本文采用基于放松TP模型转换的控制设计框架,该框架支持TP模型表示和凸包操作的复杂性和精度权衡,可在待导出的控制系统的所有组件上单独执行。对于系统的所有组件都以TP模型形式处理的常见情况,本文还建议对框架进行一些专门化和进一步放宽。该框架还扩展了TP模型插值技术,以执行系统的凸包操作。对包含Stribeck摩擦的三自由度气动弹性翼截面模型的复杂NATA模型进行了全面的研究。通过算例证明,复杂性和凸壳对设计的可行性都有很大影响。进一步证明了给定模型的单独凸包操作对于控制器和观测器的设计也是必须考虑的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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