Small-Time Local Controllability of the Orientation of a Spacecraft actuated by CMGs-Reference-Cited by-同舟云学术

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Small-Time Local Controllability of the Orientation of a Spacecraft actuated by CMGs

Published:2011-01 Issue:1 Volume:44 Page:13828-13833
ISSN:1474-6670
Container-title:IFAC Proceedings Volumes
language:en
Short-container-title:IFAC Proceedings Volumes

Author:

Bayadi Ramaprakash,Banavar Ravi N.,Maschke Bernhard M.

Publisher

Elsevier BV

Subject

General Medicine

Reference7 articles.

1. Geometric theory of single gimbal control moment gyroscope systems;Murguiles;Journal of astronautical sciences,1978

2. Controllability of spacecraft attitude using control moment gyroscopes;Bhat;IEEE Transactions on Automatic Control,2009

3. Survey of theory and steering laws of single gimbal control moment gyros;Kurokawa;Journal of guidance, control and dynamics,2007

4. Analytical mechanics of aerospace systems;Schaub;Kluwer,2002

5. Feedback control and steering laws for spacecraft using single gimbal control moment gyroscopes;Oh;Journal of astronautical sciences,1991

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Small-time local controllability of spacecraft attitude using control moment gyros;Automatica;2015-03

2. Local controllability and stabilization of spacecraft attitude by two single-gimbal control moment gyros;Chinese Journal of Aeronautics;2013-10

3. Large Angle Maneuvers of Spacecraft Based on Singularity Avoidance of SGCMGs;AIAA Guidance, Navigation, and Control (GNC) Conference;2013-08-15

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