Maximum Null Motion Algorithm for Single Gimbal Control Moment Gyroscopes-Reference-Cited by-同舟云学术

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Maximum Null Motion Algorithm for Single Gimbal Control Moment Gyroscopes

Published:2017-12-15 Issue: Volume: Page:689-707
ISSN:
Container-title:Advances in Aerospace Guidance, Navigation and Control
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Author:

Schallig S. A. V.,Chu Q. P.,Rhee S. W.,van Kampen E.

Publisher

Springer International Publishing

Link

http://link.springer.com/content/pdf/10.1007/978-3-319-65283-2_37

Reference19 articles.

1. Bedrossian NS, Paradiso J, Stark C, Rowell D (1990) Steering law design for redundant single-gimbal control moment gyroscopes. J Guid Control Dyn 13(6):1083–1089

2. Chubb W, Seltzer S (1971) Skylab attitude and pointing control system. NASA TN D-6068 (February). http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19710007043.pdf

3. Clark C, Worrall K, Yavuzoglu E (2010) A control moment gyro for dynamic attitude control of small satellites conference on small satellites. In: AIAA/USU conference on small satellites. http://digitalcommons.usu.edu/smallsat/2010/all2010/68/

4. Crassidis JL, Markley FL, Cheng Y (2007) Survey of nonlinear attitude estimation methods. J Guid Control Dyn 30(1):12–28. https://doi.org/10.2514/1.22452

5. Ford KA, Hall CD (2000) Singular direction avoidance steering for control-moment gyros. J Guid Control Dyn 23(4):648–656. https://doi.org/10.2514/2.4610

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1. Momentum Space Analysis for Mixed Skew Angle Arrays;Advances in Spacecraft Attitude Control;2020-01-15

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