DocumentCode
2103232
Title
Some solutions of a rigid body attitude under one failure mode
Author
Siguerdidjane, H.B.
Author_Institution
Lab. des Signaux et Syst., Ecole Superieure d´´Electr., Gif-sur-Yvette, France
fYear
1993
fDate
15-17 Dec 1993
Firstpage
1478
Abstract
This paper deals with the motion of a rigid body under only one failure mode. The formulation of the closed loop exact solution of the angular momentum components leads to the applied smooth feedback as well as the solution of Euler angles and the stability conditions. The case where the rigid spacecraft, using gas jet, operates in the presence of one failure mode is considered
Keywords
aerospace control; attitude control; closed loop systems; feedback; space vehicles; stability; Euler angles; angular momentum; closed loop exact solution; failure mode; rigid body attitude; rigid spacecraft; smooth feedback; stability conditions; Actuators; Angular velocity; Angular velocity control; Control systems; Eigenvalues and eigenfunctions; Feedback loop; Nonlinear equations; Space vehicles; Stability; Torque control;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1993., Proceedings of the 32nd IEEE Conference on
Conference_Location
San Antonio, TX
Print_ISBN
0-7803-1298-8
Type
conf
DOI
10.1109/CDC.1993.325433
Filename
325433
Link To Document