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Simplified Singularity Avoidance Using Variable-Speed Control Moment Gyroscope Null Motion

  • Published:2009-11 Issue:6 Volume:32 Page:1938-1943
  • ISSN:0731-5090
  • Container-title:Journal of Guidance, Control, and Dynamics
  • language:en
  • Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

McMahon Jay1,Schaub Hanspeter1

Affiliation:

1. University of Colorado at Boulder, Boulder, Colorado 80309-0431

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Cited by 19 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. Unwinding-Free Fast Finite-Time Sliding Mode Satellite Attitude Tracking Control;Journal of Guidance, Control, and Dynamics;2023-02

2. Optimizing Designed Variable Speed Control Moment Gyroscopes with Variable Skew Angle;Journal of Applied Mathematics and Physics;2023

3. Attitude control for spacecraft using pyramid-type variable-speed control moment gyros;Acta Astronautica;2020-08

4. Developments of attitude determination and control system of microsats: A survey;Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering;2020-01-06

5. Variable Speed Control Moment Gyroscope in an Inverted Pendulum;Journal of Dynamic Systems, Measurement, and Control;2019-09-18
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