DocumentCode
2252604
Title
Guaranteed cost control of stochastic uncertain systems applied to a problem of missile autopilot design
Author
Petersen, Ian R.
Author_Institution
Dept. of Electr. Eng., Australian Defence Force Acad., Canberra, ACT, Australia
Volume
3
fYear
1998
fDate
21-26 Jun 1998
Firstpage
1737
Abstract
We apply a result on output feedback guaranteed cost control of stochastic uncertain systems to the problem of designing a missile autopilot. In the missile autopilot design problem, the given data is a finite collection of plant models for the missile corresponding to different flight conditions. A total least squares approach is used to fit the data to a norm bounded uncertain system model
Keywords
control system synthesis; cost optimal control; feedback; least squares approximations; missile guidance; robust control; stochastic systems; uncertain systems; flight conditions; missile autopilot design; norm bounded uncertain system model; output feedback guaranteed cost control; stochastic uncertain systems; total least squares approach; Control systems; Costs; Missiles; Optimal control; Output feedback; Robust control; Stochastic resonance; Stochastic systems; Uncertain systems; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1998. Proceedings of the 1998
Conference_Location
Philadelphia, PA
ISSN
0743-1619
Print_ISBN
0-7803-4530-4
Type
conf
DOI
10.1109/ACC.1998.707304
Filename
707304
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