Active fault tolerant control scheme for satellite attitude system subject to actuator time‐varying faults
Author:
Affiliation:
1. College of Automation, Nanjing University of Posts and TelecommunicationsNanjing210046People's Republic of China
2. College of Electrical Engineering and Control Science, Nanjing Tech UniversityNanjing211800People's Republic of China
Funder
National Natural Science Foundation of China
Publisher
Institution of Engineering and Technology (IET)
Subject
Electrical and Electronic Engineering,Control and Optimization,Computer Science Applications,Human-Computer Interaction,Control and Systems Engineering
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1049/iet-cta.2017.0969
Reference44 articles.
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4. Sliding mode fault tolerant tracking control for a flexiable hypersonic vehicle with actuator faults;Gao Z.F.;ICIC Express Lett. B, Appl.,2015
5. Robust FDI applied to thruster faults of a satellite system
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