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
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;
Conference_Titel :
American Control Conference, 1993
Conference_Location :
San Francisco, CA, USA
Print_ISBN :
0-7803-0860-3
