Closed-Loop-Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Fault
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
2. University of Texas at Austin, Austin, Texas 78712-1221
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.G003028
Reference36 articles.
1. Bibliographical review on reconfigurable fault-tolerant control systems
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