Steering Law of Control Moment Gyros using Optimization of Initial Gimbal Angles for Satellite Attitude Control
Author:
Affiliation:
1. School of Science for Open and Environment Systems, Keio University
Publisher
Japan Society of Mechanical Engineers
Link
http://www.jstage.jst.go.jp/article/jsdd/5/1/5_1_30/_pdf
Reference10 articles.
1. (1) Nakamura, Y., and Hanafusa, H., Inverse Kinematic Solutions with Singularity Robustness for Robot Manipulator Control, Journal of Dynamic Systems, Measurement, and Control, Vol.108, 1986, pp.163-171.
2. (2) Wie, B., Singularity Robust Steering Logic for Redundant Single-Gimbal Control Moment Gyros, Journal of Guidance, Control, and Dynamics, Vol.24, No.5, 2001, pp.865-872.
3. (3) Wie, B., Space Vehicle Dynamics and Control, AIAA Education Series, pp.419-450.
4. (4) Vadali, S. R., Krishnan, S., Suboptional Command Generation for Control Moment Gyroscopes and Feedback Control of Spacecraft, Journal of Guidance, Control, and Dynamics, Vol.18, No.6, 1995, pp.1350-1354.
5. (5) Kawai, H., Maneuver Simulation of a Spacecraft Considering CMG Gimbal Axis Torques, JAXA Research and Development Memorandum, 2004.
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