Attitude stabilization of a rigid spacecraft using two momentum wheel actuators
Author:
Affiliation:
1. National University of Singapore, 0511 Singapore
2. University of Michigan, Ann Arbor, Michigan 48109-2140
3. King Fahd University of Petroleum and Minerals, Dhahran 31261, Saudi Arabia
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/10.2514/3.21378
Reference35 articles.
1. Variable-structure control of spacecraft large-angle maneuvers
2. The attitude control problem
3. Quaternion feedback for spacecraft large angle maneuvers
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