DocumentCode :
1600835
Title :
Robust full-envelope missile autopilot design
Author :
Juang, Jyh-Ching ; Lin, Ching-Fang ; Cloutier, James R. ; Evers, Johnny H.
Author_Institution :
American GNC Corp., Chatsworth, CA, USA
fYear :
1992
Firstpage :
231
Abstract :
The design of a robust full-envelope autopilot for the HAVE DASH II missile system is delineated. Existing control design methods are examined and integrated to meet the stringent performance requirements of the missile autopilot design
Keywords :
control system synthesis; missiles; stability; HAVE DASH II missile system; control design methods; performance requirements; robust full-envelope autopilot; Aerodynamics; Design methodology; Missiles; Observability; Robust control; Robust stability; Robustness; Uncertainty; Velocity control; Virtual manufacturing;
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.1992.269871
Filename :
269871
Link To Document :
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