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