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Suboptimal controller design for flexible launch vehicle based on genetic algorithm: Selection of the weighting matrices Q and R

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

In this study, a suboptimal controller for the pitch plane motion of a flexible launch vehicle is presented. Three sensors for measuring the motion, angular position sensor, angular rate sensor and accelerometer, are considered and assumed to be at given positions on a rocket described by a ninth-order state-space dynamical model, including three bending modes. The weighting matrices with respect to the suboptimal control method, which are used to synthesize a performance index, are selected by the genetic algorithm. Additionally, in order to improve the robust performance of the flexible launch vehicle, various uncertainty combinations are predetermined and considered in the process of the genetic search. The simulation results indicate that both the rigid body and flexible mode response are desirable, and the control performance including the robust performance is better than that of the suboptimal controller with manual selection of the weighting matrices.

源语言英语
主期刊名Proceedings - 2009 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2009
720-724
页数5
DOI
出版状态已出版 - 2009
活动2009 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2009 - Shanghai, 中国
期限: 20 11月 200922 11月 2009

出版系列

姓名Proceedings - 2009 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2009
2

会议

会议2009 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2009
国家/地区中国
Shanghai
时期20/11/0922/11/09

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