DocumentCode :
1695968
Title :
Design of Guidance Law for Homing Missile Via Feedback Linearization
Author :
Bezick, Scott ; Rusnak, Ilan ; Gray, W. Steven
Author_Institution :
Department of Electrical and Computer Engineering, Drexel University, PA
fYear :
1993
Firstpage :
729
Lastpage :
733
Keywords :
Acceleration; Control system synthesis; Control systems; Feedback; Geometry; Kinematics; Missiles; Navigation; Nonlinear control systems; Virtual manufacturing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Control Systems, 1993. Proceedings. The First IEEE Regional Conference on
Type :
conf
DOI :
10.1109/AEROCS.1993.721029
Filename :
721029
Link To Document :
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