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
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;
Conference_Titel :
American Control Conference, 1998. Proceedings of the 1998
Conference_Location :
Philadelphia, PA
Print_ISBN :
0-7803-4530-4
DOI :
10.1109/ACC.1998.707304
