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
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;
Conference_Titel :
Decision and Control, 1993., Proceedings of the 32nd IEEE Conference on
Conference_Location :
San Antonio, TX
Print_ISBN :
0-7803-1298-8
DOI :
10.1109/CDC.1993.325433
