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
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2003年 / 26卷 / 06期
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.
引用
收藏
页码：914 / 917
页数：4
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