Adaptive Direct Compensation Control Scheme for Spacecraft with Multiple Actuator Faults
Author:
Affiliation:
1. Nanjing University of Aeronautics and Astronautics, 211106 Nanjing, People’s Republic of China
2. University of Virginia, Charlottesville, Virginia 22903
Funder
National Natural Science Foundation of China
Natural Science Foundation of Jiangsu Province of China
Nanjing University of Aeronautics and Astronautics Research Foundation for the third author’s visiting professorship
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
https://arc.aiaa.org/doi/pdf/10.2514/1.G003661
Reference26 articles.
1. Bibliographical review on reconfigurable fault-tolerant control systems
2. Adaptive Control of Systems with Actuator Failures
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