MIXED H-2/H-INFINITY

被引:10
|
作者
SCHOMIG, E
SZNAIER, M
LY, UL
机构
[1] PENN STATE UNIV,UNIVERSITY PK,PA 16802
[2] UNIV WASHINGTON,DEPT AERONAUT & ASTRONAUT,SEATTLE,WA 98195
关键词
D O I
10.2514/3.21418
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this paper vie consider the problem of minimizing a nominal H-2 performance measure subject to robust stability constraints for systems having multiple operating points. Performance is measured in terms of a weighted sum of the individual H-2 norms at each plant condition, whereas robust stability is enforced through H-infinity-norm bounds. The problem is solved by considering a new time-domain scalar cost function J(infinity) (t(f)) that incorporates the H-infinity constraints into a single cost function. Using the proposed formulation, the mixed H-2/H-infinity design problem becomes an unconstrained optimization problem that, for t(f) --> infinity, recovers the original objective of minimizing the performance measure subject to the given H-infinity bounds. The resulting optimization problem is smooth, and hence standard gradient-based software can be applied. Moreover, this formulation allows for the synthesis of linear time-invariant controllers having a prespecified order and structure. The method is illustrated by the design of a single first-order controller for the pitch stability augmentation system of an F-15 aircraft operating at both subsonic and supersonic flight conditions.
引用
收藏
页码:525 / 531
页数:7
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