DocumentCode
1598549
Title
Advanced control for the design of STT missile autopilots
Author
Bendotti, P. ; Saad, M.M.
Author_Institution
Div. des Engins Tactiques, Aerospatiale, Chatillon-sous-Bagneux, France
fYear
1992
Firstpage
613
Abstract
Presented is an application of adaptive control techniques to the design of skid-to-turn (STT) missile autopilots. The adaptive controller is obtained by combining a multivariable linear-quadratic control design with a parameter estimator robust with respect to relatively large aerodynamic variations and modeling errors. Realistic simulations involving a physical model of a STT missile are reported to demonstrate the performance and stability robustness of the autopilot
Keywords
adaptive control; aerospace control; control system synthesis; missiles; multivariable control systems; optimal control; parameter estimation; stability; STT missile autopilots; adaptive control; multivariable linear-quadratic control; parameter estimator; robustness; skid-to-turn missiles; stability; Adaptive control; Aerodynamics; Aerospace control; Aerospace industry; Control design; Missiles; Parameter estimation; Programmable control; Robust control; Stability analysis;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 1992., First IEEE Conference on
Conference_Location
Dayton, OH
Print_ISBN
0-7803-0047-5
Type
conf
DOI
10.1109/CCA.1992.269778
Filename
269778
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