DocumentCode
1694693
Title
Application of Sliding Mode Control to Bank-To-Turn Missile Systems
Author
Huang, J. ; Lin, C.F.
Author_Institution
American GNC Corporation, CA
fYear
1993
Firstpage
569
Lastpage
573
Keywords
Control system synthesis; Control systems; Degradation; Design methodology; Linear feedback control systems; Missiles; Optimal control; Robust control; Sliding mode control; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Control Systems, 1993. Proceedings. The First IEEE Regional Conference on
Type
conf
DOI
10.1109/AEROCS.1993.720998
Filename
720998
Link To Document