Title :
Application of Sliding Mode Control to Bank-To-Turn Missile Systems
Author :
Huang, J. ; Lin, C.F.
Author_Institution :
American GNC Corporation, CA
Keywords :
Control system synthesis; Control systems; Degradation; Design methodology; Linear feedback control systems; Missiles; Optimal control; Robust control; Sliding mode control; Uncertainty;
Conference_Titel :
Aerospace Control Systems, 1993. Proceedings. The First IEEE Regional Conference on
DOI :
10.1109/AEROCS.1993.720998
