Indirect Robust Adaptive Fault -Tolerant Control for Attitude Tracking of Spacecraft
Author:
Affiliation:
1. North Carolina A&T State University, Greensboro, North Carolina 27411
2. Volvo North American, Inc., Greensboro, North Carolina 27455
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/10.2514/1.31158
Reference22 articles.
1. Nonlinear Attitude State Tracking Control for Spacecraft
2. The attitude control problem
3. Variable-structure control of spacecraft large-angle maneuvers
4. Inverse optimal stabilization of a rigid spacecraft
5. Inverse optimal adaptive control for attitude tracking of spacecraft
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