DocumentCode
335594
Title
Nonlinear Quaternion Feedback Control For Spacecraft Via Angular Velocity Shaping
Author
Lu, Jianbo ; Wie, Bong
Author_Institution
Purdue University
Volume
1
fYear
1994
fDate
29 June-1 July 1994
Firstpage
632
Lastpage
636
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;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1994
Print_ISBN
0-7803-1783-1
Type
conf
DOI
10.1109/ACC.1994.753446
Filename
753446
Link To Document