Underactuated Spacecraft Switching Law for Two Reaction Wheels and Constant Angular Momentum
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan, 48109
2. U.S. Air Force Research Laboratory, Kirtland Air Force Base, Albuquerque, New Mexico 87117
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.G001680
Reference19 articles.
1. Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models
2. Overview of the [ITAL]Far Ultraviolet Spectroscopic Explorer[/ITAL] Mission
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4. On the attitude stabilization of rigid spacecraft
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