Inertia-Free Spacecraft Attitude Tracking with Disturbance Rejection and Almost Global Stabilization
Author:
Affiliation:
1. University of Hawaii at Manoa, Honolulu, Hawaii 96822
2. U.S. Air Force Research Laboratory, Kirtland Air Force Base, New Mexico 87117
3. Robert Bosch LLC, Palo Alto, California 94304
4. University of Michigan, Ann Arbor, Michigan 48109
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/10.2514/1.41565
Reference27 articles.
1. Stabilization and optimality results for the attitude control problem
2. Optimal Nonlinear Tracking of Spacecraft Attitude Maneuvers
3. A topological obstruction to continuous global stabilization of rotational motion and the unwinding phenomenon
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