State-dependent Riccati equation for control of aeroelastic flutter

被引:16
|
作者
Tadi, M [1 ]
机构
[1] Univ Colorado, Dept Mech Engn, Denver, CO 80202 USA
关键词
D O I
10.2514/2.6918
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Feedback control design for suppression of flutter in an aeroelastic system is studied. Feedback control laws based on the state-dependent Riccati equation are derived. Two control laws are studied: one formulation uses an observer to estimate the states after which it uses the estimated states to generate feedback law; the other formulation uses partial observation to directly generate the control law.
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页码:914 / 917
页数:4
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