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