Generalized Predictive Control for Spacecraft Attitude Based on Adaptive Fuzzy Estimator
Publication: Journal of Aerospace Engineering
Volume 30, Issue 5
Abstract
A generalized predictive control with adaptive fuzzy estimator (GPC-AFE) is proposed for spacecraft. Model uncertainties and mismatch disturbances are considered in the process of controller design. For the attitude subsystem, a predictive control based on an adaptive fuzzy estimator is designed to deal with the unknown disturbances. For the angular velocity subsystem, the actual control input is designed by using the generalized predictive control. The derivative of virtual control and unknown disturbances in the actual control are also estimated by using an adaptive fuzzy estimator. With the proposed generalized predictive control, the tracking error of the attitude converges to a bounded neighborhood of the reference attitude. Theoretical results are illustrated by numerical simulation.
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Published In
Journal of Aerospace Engineering
Volume 30 • Issue 5 • September 2017
Copyright
©2017 American Society of Civil Engineers.
History
Received: Apr 9, 2016
Accepted: Jan 6, 2017
Published online: Mar 24, 2017
Discussion open until: Aug 24, 2017
Published in print: Sep 1, 2017
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