Redundant Reaction Wheel Torque Distribution Yielding Instantaneous L2 Power-Optimal Spacecraft Attitude Control
Author:
Affiliation:
1. University of Colorado at Boulder, Boulder, Colorado 80309
2. Surrey Space Centre, Guildford, Surrey, GU2 7XH, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.41070
Reference30 articles.
1. Spin-axis stabilization of symmetric spacecraft with two control torques
2. Exact nonlinear control of spacecraft slewing maneuvers with internal momentum transfer
3. Essentially Globally Asymptotically Stable Nutation Control Using a Single Reaction Wheel
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