Integral Sliding Mode Fault-Tolerant Control for Spacecraft With Uncertainties and Saturation
Author:
Affiliation:
1. Beijing Institute of Control Engineering; Beijing China
Publisher
Wiley
Subject
Control and Systems Engineering
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1002/asjc.1365/fullpdf
Reference25 articles.
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4. Fault tolerant small satellite attitude control using adaptive non-singular terminal sliding mode;Cao;Adv. Space Res.,2013
5. A direct adaptive actuator failure compensation scheme for satellite attitude control systems;Ma;Proceeding of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,2014
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