DocumentCode :
1695522
Title :
Missile Autopilot Design Using a Generalized Hamiltonian Formulation
Author :
Lin, Ching-Fang ; Cloutier, James R. ; Evers, Johnny H.
Author_Institution :
American GNC Corporation, CA
fYear :
1993
Firstpage :
715
Lastpage :
723
Keywords :
Aerodynamics; Algorithm design and analysis; Bandwidth; Degradation; Design methodology; Force control; Kinematics; Missiles; Robust control; Robustness;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Control Systems, 1993. Proceedings. The First IEEE Regional Conference on
Type :
conf
DOI :
10.1109/AEROCS.1993.721027
Filename :
721027
Link To Document :
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