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
fDate :
1/1/1993 12:00:00 AM
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;
Journal_Title :
Automatic Control, IEEE Transactions on
