Inverse Optimal Attitude Stabilization of Flexible Spacecraft with Actuator Saturation

This paper presents a new robust inverse optimal control strategy for flexible spacecraft attitude maneuvers in the presence of external disturbances and actuator constraint. A new constrained attitude controller for flexible spacecraft is designed based on the Sontag-type formula and a control Lyap...

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Bibliographic Details
Main Author: Chutiphon Pukdeboon
Format: Article
Language:English
Published: Hindawi Limited 2016-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2016/1395952