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基于LMI的降阶鲁棒控制器设计 被引量:1

Robust Reduced-Order Controller Design Based on LMI
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摘要 基于线性矩阵不等式 (LMI)的H∞ 设计方法给出了所有全阶和降阶控制器的参数化结果 ,其中降阶控制器的求解需要满足一个秩条件 ,这个秩条件是非凸的 .为了避开非凸问题的求解 ,提出了一种新的设计降阶控制器的凸优化方法 ,从而得到了保证H∞ 性能指标的降阶控制器 .为了减少保守性 ,进而基于投影原理提出了一种设计更低阶次鲁棒控制器的新方法 .该方法为系统的H∞ A non convex problem has to be solved in the designing of reduced order H ∞ controller based on linear matrix inequality(LMI), which is so far an open problem. In this paper, a new method is presented to design reduced order H ∞ contrller with convex optimization. It guarantees H ∞ performance, but some conservation may be introduced. In order to decrease the conservation, the projection principle is used. Thus, a lower order robust controller can be obtained but the H ∞ performance may not be guaranteed. It is a trade off between the order of controller and the H ∞ performance in practice. Generally, if the projection error is small enough, the design result could be satisfied. The simulation results illustrate the advantages of this method.
出处 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2000年第6期722-725,共4页 Journal of Beijing University of Aeronautics and Astronautics
基金 高等学校博士学科点专项科研基金资助项目! (96 0 3)
关键词 线性矩阵不等式 LMI 降阶鲁棒控制器 设计 regulator problems suboptimal control controllers linear matrix inequality(LMI) H ∞ control reduced order controller design
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参考文献4

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同被引文献5

  • 1Walker B, Saraf A, Godbole A. Robust flight control for coordinated turns[ R]. AIAA-2003-5553,2003.
  • 2Wichai Siwakosit. Robust and reconfigurable flight control system design [ J ]. Mechanical and Aeronautical Engineering, 2001,62(7) :110-114.
  • 3Rozak J N, Ray A. Robust multivariable control of rotorcraft in forward flight [ J]. Journal of the American Helicopter Society, 1997 ,42(2) :149 - 160.
  • 4David Cabecinhas, Carlos Silvestre,Paulo Rosa, et al. Path-following control for coordinated turn aircraft maneuvers [R]. AIAA-2007-6656,2007.
  • 5白蒲江,王新民,余翔,李俨.基于迭代LMI的直升机协调转弯控制律设计[J].测控技术,2008,27(7):86-88. 被引量:4

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