DocumentCode :
307058
Title :
Application of nonlinear H control to autopilot design
Author :
Lin, Ching-Fang ; Ge, Jian-Hua
Author_Institution :
American GNC Corp., Chatsworth, CA, USA
Volume :
3
fYear :
1996
fDate :
11-13 Dec 1996
Firstpage :
3276
Abstract :
This paper addresses the problems of nonlinear H controller design for autopilot design. A systematic procedure to find Taylor series approximations to the solutions of the Hamilton-Jacobi-Isaacs (HJI) equation is proposed. The effectiveness of the proposed nonlinear H control design approach is demonstrated by using the HAVE DASH II bank-to-turn missile autopilot as an example
Keywords :
H control; MIMO systems; approximation theory; control system synthesis; missile guidance; nonlinear control systems; series (mathematics); H control; HAVE DASH II bank-to-turn missile; Hamilton-Jacobi-Isaacs equation; MIMO systems; Taylor series approximations; autopilot design; nonlinear control; Aerodynamics; Control nonlinearities; Control systems; Control theory; Missiles; Nonlinear control systems; Nonlinear equations; Stability; Taylor series; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1996., Proceedings of the 35th IEEE Conference on
Conference_Location :
Kobe
ISSN :
0191-2216
Print_ISBN :
0-7803-3590-2
Type :
conf
DOI :
10.1109/CDC.1996.573647
Filename :
573647
Link To Document :
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