Title :
Nonlinear Quaternion Feedback Control For Spacecraft Via Angular Velocity Shaping
Author :
Lu, Jianbo ; Wie, Bong
Author_Institution :
Purdue University
fDate :
29 June-1 July 1994
Abstract :
A nonlinear feedback control logic is developed for a spacecraft attitude control through angular velocity shaping in time domain. The proposed control logic guarantees slew rate constraint and can tolerate uncertainties in the inertia matrix.
Keywords :
Angular velocity; Angular velocity control; Equations; Feedback control; Logic; Motion control; Quaternions; Space vehicles; Uncertainty; Velocity control;
Conference_Titel :
American Control Conference, 1994
Print_ISBN :
0-7803-1783-1
DOI :
10.1109/ACC.1994.753446
