Abstract
To solve the rigid spacecraft attitude maneuver problem, an adaptive fuzzy fault-tolerant sliding mode controller is designed. The controller is based on the terminal sliding mode scheme. The adaptive learning algorithm and the fuzzy logic system are designed to estimate the attitude tracking dynamics. The stability of the controller is proved by Lyapunov method. Finite-time convergence of spacecraft attitude orientation to the neighborhood of the equilibrium point is obtained. Finally, a numerical simulation is employed to illustrate the advantages of the proposed controller. Simulation results confirm that the designed controller yields high control precision and great fault-tolerant capability.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callMore From: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
