Necessary and sufficient conditions for H-∞ static output-feedback control

被引:95
作者
Gadewadikar, Jyotirmay
Lewis, Frank L.
Abu-Khalaf, Murad
机构
[1] Univ Texas Arlington, Automat & Robot Res Inst, Ft Worth, TX 76118 USA
[2] Univ Texas Arlington, Dept Elect Engn, Ft Worth, TX 76118 USA
基金
美国国家科学基金会;
关键词
D O I
10.2514/1.16794
中图分类号
V [航空、航天];
学科分类号
08 [工学]; 0825 [航空宇航科学与技术];
摘要
Necessary and sufficient conditions are presented for static output-feedback control of linear time-invariant systems using the H-infinity approach. Simplified conditions are derived which only require the solution of two coupled matrix design equations. It is shown that the static output-feedback H-infinity solution does not generally yield a well-defined saddle point for the zero-sum differential game; conditions are given under which it does. This paper also proposes a numerically efficient solution algorithm for the coupled design equations to determine the output-feedback gain. A major contribution is that an initial stabilizing gain is not needed. An F-16 normal acceleration design example is solved to illustrate the power of the proposed approach.
引用
收藏
页码:915 / 920
页数:6
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