Convex Optimization for Power Tracking of Double-Gimbal Variable-Speed Control Moment Gyroscopes
Author:
Affiliation:
1. Osaka Prefecture University, Sakai 599-8531, Japan
2. University of Colorado, Boulder, Colorado 80309
Funder
Japan Society for the Promotion of Science
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33944
Reference33 articles.
1. CormackA. III, “Three Axis Flywheel Energy and Control Systems,” NASA TN-73-G&C-8, 1973.
2. Satellite Attitude Control and Power Tracking with Energy/Momentum Wheels
3. Spacecraft Adaptive Attitude and Power Tracking with Variable Speed Control Moment Gyroscopes
4. JungD.TsiotrasP. “An Experimental Validation of Spacecraft Attitude and Power Tracking with Variable Speed Control Moment Gyroscopes,” 17th AAS/AIAA Space Flight Mechanics Meeting, AAS Paper 07-130, Sedona, AZ, Jan.–Feb. 2007.
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