By Topic

Exact feedback linearization and control of space station using CMG

Sign In

Cookies must be enabled to login.After enabling cookies , please use refresh or reload or ctrl+f5 on the browser for the login options.

Formats Non-Member Member
$31 $13
Learn how you can qualify for the best price for this item!
Become an IEEE Member or Subscribe to
IEEE Xplore for exclusive pricing!
close button

puzzle piece

IEEE membership options for an individual and IEEE Xplore subscriptions for an organization offer the most affordable access to essential journal articles, conference papers, standards, eBooks, and eLearning courses.

Learn more about:

IEEE membership

IEEE Xplore subscriptions

2 Author(s)
Singh, S.N. ; Dept. of Electr. & Comput. Eng., Nevada Univ., Las Vegas, NV, USA ; Bossart, T.C.

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

Published in:

Automatic Control, IEEE Transactions on  (Volume:38 ,  Issue: 1 )