Selecting Initial Gimbal Angles of Roof-type CMG System for Avoiding Singularities in Spacecraft Attitude Maneuver-Reference-Cited by-同舟云学术

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Selecting Initial Gimbal Angles of Roof-type CMG System for Avoiding Singularities in Spacecraft Attitude Maneuver

Published:2022 Issue:3 Volume:65 Page:123-133
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

LIU Haoxiang¹,SATOH Satoshi²,SHOJI Yasuhiro³,JIKUYA Ichiro⁴,YAMADA Katsuhiko²

Affiliation:

1. Department of Mechanical, Materials and Manufacturing Science, Osaka University

2. Department of Mechanical Engineering, Osaka University

3. Advanced Research Center for Space Science and Technology, Institute of Science and Engineering, Kanazawa University

4. Faculty of Frontier Engineering, Institute of Science and Engineering, Kanazawa University

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/65/3/65_T-21-24/_pdf

Reference12 articles.

1. 1) Wie, B.: Singularity Analysis and Visualization for Single-Gimbal Control Moment Gyro Systems, J. Guid. Control Dynam., 27 (2004), pp. 271–282.

2. 2) Kurokawa, H.: Survey of Theory and Steering Laws of Single-Gimbal Control Moment Gyros, J. Guid. Control Dynam., 30 (2007), pp. 1331–1340.

3. 3) Ford, K. A. and Hall, C. D.: Singular Direction Avoidance Steering for Control-Moment Gyros, J. Guid. Control Dynam., 23 (2000), pp. 648–656.

4. 4) Wie, B., Bailey, D., and Heiberg, C.: Singularity Robust Steering Logic for Redundant Single-Gimbal Control Moment Gyros, J. Guid. Control Dynam., 24 (2001), pp. 865–872.

5. 5) Schaub, H. and Junkins, J.: Singularity Avoidance Using Null Motion and Variable-Speed Control Moment Gyros, J. Guid. Control Dynam., 23 (2000), pp. 11–16.

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