Maneuverability Analysis-Based Attitude Control of Spacecraft with Two Pairs of Two-Parallel Control Moment Gyroscopes
Author:
Affiliation:
1. Department of Aerospace Engineering, Chosun University
2. Department of Aerospace Engineering and Engineering Mechanics, University of Cincinnati
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/tjsass/67/4/67_T-22-42/_pdf
Reference9 articles.
1. 1) Yoon, H. and Tsiotras, P.: Spacecraft Adaptive Attitude and Power Tracking with Variable Speed Control Moment Gyroscopes, J. Guid. Control Dynam., 25, 6 (2002), pp. 1081–1090.
2. 2) Schaub, H. and Junkins, J. L.: Analytical Mechanics of Space Systems, AIAA, 2003.
3. 3) Leve, F. A., Hamilton, B. J., and Peck, M. A.: Spacecraft Momentum Control Systems, Springer, Vol. 1010, 2015.
4. 4) Schaub, H. and Junkins, J. L.: Singularity Avoidance Using Null Motion and Variable-speed Control Moment Gyros, J. Guid. Control Dynam., 23, 1 (2000), pp. 11–16.
5. 5) Yoon, H. and Tsiotras, P.: Singularity Analysis of Variable Speed Control Moment Gyros, J. Guid. Control Dynam., 27, 3 (2004), pp. 374–386.
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