Active fault-tolerant attitude control for flexible spacecraft with loss of actuator effectiveness
Author:
Affiliation:
1. Department of Control Science and Engineering; Harbin Institute of Technology; Harbin 150001 China
2. College of Engineering; Swansea University; Singleton Park, Swansea SA2 8PP UK
Publisher
Wiley
Subject
Electrical and Electronic Engineering,Signal Processing,Control and Systems Engineering
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1002/acs.2363/fullpdf
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