DocumentCode
835078
Title
Exact feedback linearization and control of space station using CMG
Author
Singh, Sahjendra N. ; Bossart, Theodore C.
Author_Institution
Dept. of Electr. & Comput. Eng., Nevada Univ., Las Vegas, NV, USA
Volume
38
Issue
1
fYear
1993
fDate
1/1/1993 12:00:00 AM
Firstpage
184
Lastpage
187
Abstract
Based on feedback linearization theory, an approach to attitude control of a space station using control moment gyros (CMGs) is developed. A linearizing transformation is derived to obtain a simple linear representation of the nonlinear pitch axis dynamics. A feedback control law for trajectory tracking is derived. Extension of this approach to linearization of the coupled yaw and roll axis dynamics and control is presented
Keywords
aerospace control; attitude control; feedback; linearisation techniques; space vehicles; aerospace control; attitude control; control moment gyros; exact feedback linearisation; nonlinear pitch axis dynamics; space station; trajectory tracking; Angular velocity; Control systems; Differential equations; Feedback control; Linear feedback control systems; Nonlinear dynamical systems; Nonlinear equations; Space stations; Space vehicles; Vehicle dynamics;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/9.186337
Filename
186337
Link To Document