Attitude Stabilization of a Spacecraft by Two Skew Single-Gimbal Control Moment Gyros-Reference-Cited by-同舟云学术

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Attitude Stabilization of a Spacecraft by Two Skew Single-Gimbal Control Moment Gyros

Published:2013-08-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control (GNC) Conference
language:
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Author:

Gui Haichao¹,Jin Lei¹,Xu Shijie¹,Hu Quan¹

Affiliation:

1. Beihang University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-4794

Reference45 articles.

1. Feedback Control Law for Variable Speed Control Moment Gyros

2. Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models

3. 5Keraï,E.L."AnalysisofSmallTime LocalControllabilityofthe RigidBodyModel,"Proceedings oftheIFACSymposium on System Structureand Control, Nantes, France,1995, pp.597-602.

Cited by 7 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. Backstepping-Based Steering Control for Spacecraft Attitude Control Using Two-Skewed Control Moment Gyroscopes;Journal of Guidance, Control, and Dynamics;2023-01

2. Attitude Stabilization of a Spacecraft with Two Parallel Control Moment Gyroscopes;Journal of Guidance, Control, and Dynamics;2016-03

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

4. Attitude Tracking Control of a Spacecraft by Two Reaction Wheels;AIAA Guidance, Navigation, and Control Conference;2015-01-02

5. On the attitude stabilization of a rigid spacecraft using two skew control moment gyros;Nonlinear Dynamics;2014-11-20

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