DocumentCode
490070
Title
Sliding Mode Control of HAVE DASH II Missile Systems
Author
Huang, J. ; Lin, C.F.
Author_Institution
American GNC Corporation, 9131 Mason Ave., Chatsworth, CA 91311
fYear
1993
fDate
2-4 June 1993
Firstpage
183
Lastpage
187
Abstract
Sliding mode control is applied to design autopilot for bank-to-turn (BTT) missile systems. The design is compared with the feedback linearization approach and shows a significant improvement over the latter.
Keywords
Aerodynamics; Control systems; Design methodology; Linear feedback control systems; Missiles; Nonlinear systems; Optimal control; Process design; Sliding mode control; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1993
Conference_Location
San Francisco, CA, USA
Print_ISBN
0-7803-0860-3
Type
conf
Filename
4792833
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