发明名称 Robust spacecraft controller and method for designing same
摘要 A method, apparatus, article of manufacture, and a memory structure for designing a robust controller. The method comprises the steps of determining a plant model G of the system dynamics; bounding system dynamics unmodeled by the plant model G of the system dynamics by a weighting function W; applying a transform to an augmented plant model T having the plant model G and the weighting function W; defining a controller F from the transformed plant model T; and applying an inverse of the transform to the controller F defined from the transformed plant model and the weighting function W to generate the robust controller F.
申请公布号 US7337021(B2) 申请公布日期 2008.02.26
申请号 US20030397495 申请日期 2003.03.26
申请人 THE BOEING COMPANY 发明人 CHIANG RICHARD Y.;IH CHE-HANG CHARLES;WU YEONG-WEI ANDY
分类号 G05B13/02;G06F7/60 主分类号 G05B13/02
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