A Sequential Design Approach for Switching H∞ LPV Control

被引:2
|
作者
He, Tianyi [1 ]
Zhu, Guoming G. [2 ]
Swei, Sean S. M. [3 ]
机构
[1] Utah State Univ, Dept Mech & Aerosp Engn, Logan, UT 84322 USA
[2] Michigan State Univ, Dept Mech Engn, E Lansing, MI 48824 USA
[3] Khalifa Univ, Dept Aerosp Engn, Abu Dhabi, U Arab Emirates
关键词
Interpolated controller; PLMI; switching LPV control; synthesis complexity; AIRPLANE; LMIS;
D O I
10.1007/s12555-020-0363-3
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper proposes a sequential design scheme for switching H-infinity LPV (Linear Parameter-Varying) control, aiming to reduce the computational complexity of the associated optimization problem. Different from the traditional approach that simultaneously designs switching LPV controllers and solves a high-dimensional optimization problem, the proposed sequential design approach renders a bundle of low-dimensional optimization problems to be solved iteratively. Individual H-infinity LPV controller for each subregion is synthesized by independent PLMIs (Parametric Linear Matrix Inequalities) to guarantee H-infinity performance, and controller variables are interpolated on the overlapped subregions such that the H-infinity performance is also guaranteed on the overlapped subregion. Numerical examples are used to demonstrate the effectiveness of this method to reduce the computational load in each design iteration and improved H-infinity performance over the conventional simultaneous design method with well-tuned interpolation coefficient.
引用
收藏
页码:3354 / 3367
页数:14
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