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Please use this identifier to cite or link to this item: http://ir.ncue.edu.tw/ir/handle/987654321/13005

Title: Robust Stabilizing Digital Rocket Control
Authors: Yao, Kai-chao
Contributors: 工業教育與技術學系
Keywords: Rocket;Flight control;Robust stabilization;Optimal control;Digital
Date: 2002-11
Issue Date: 2012-08-07T01:15:52Z
Publisher: 國防大學中正理工學院;中山科學研究院;中華民國國防科技學術研究學會
Abstract: A digital rocket control technique is presented in this paper. A practical rocket ascending state model illustrates the control method. Linearization and A/D state transformation are applied to deal with the nonlinear continuous state model to the linear derivation discrete state model. The optimal control feedback and the optimal cost of the derivation variables are found based on the linearied discrete state model by constraining to the LQ performance index. Moreover, the robust stabilizing optimal feeback gain is found to stabilize the system and minimize the performance index.
Relation: 第十一屆國防科技學術研討會, 國防大學, 2002年11月14-16日
Appears in Collections:[工業教育與技術學系] 會議論文

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