Optimal desaturation of momentum exchange control systems
Author:
Affiliation:
1. University of Alabama Research Institute, Huntsville, Ala.
2. Sperry Rand Corporation, Huntsville, Ala.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6118
Reference48 articles.
1. Flywheel control of space vehicles
2. Mortensen, R. E. "Design Considerations of Inertia Wheel Systems for Attitude Control of Satellite Vehicles," Report 2313-0002-RU-OOO, Space Technology Laboratories, El Segundo, Calif.
3. Some Basic Response Relations for Reaction-Wheel Attitute Control
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