DocumentCode :
1630616
Title :
Time-varying feedback stabilization of the attitude of a rigid spacecraft with two controls
Author :
Morin, P. ; Samson, C. ; Pomet, J.-B. ; Jiang, Z.-P.
Author_Institution :
INRIA, Sophia Antipolis, France
Volume :
1
fYear :
1994
Firstpage :
914
Abstract :
Rigid body models with two controls cannot be locally asymptotically stabilized by continuous state feedbacks. Existence of a locally stabilizing smooth time-varying feedback has however been proved. Such a feedback is explicitly derived
Keywords :
aerospace control; asymptotic stability; attitude control; feedback; space vehicles; time-varying systems; continuous state feedbacks; locally asymptotically stabilized; locally stabilizing smooth time-varying feedback; rigid body models; rigid spacecraft attitude; time-varying feedback stabilization; Actuators; Angular velocity; Attitude control; Control systems; Degradation; Equations; Quaternions; Space vehicles; State feedback; Time varying systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1994., Proceedings of the 33rd IEEE Conference on
Conference_Location :
Lake Buena Vista, FL
Print_ISBN :
0-7803-1968-0
Type :
conf
DOI :
10.1109/CDC.1994.410943
Filename :
410943
Link To Document :
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