Switching Performance Optimal Controller Design for Hypersonic Vehicle Model

摘要：

This paper addresses the problem of switching performance optimal control for the longitudinal model of the generic hypersonic air-breathing flight vehicle. For the widening flight envelope of hypersonic vehicle, the multiple-mode switching control is an issue that have to be considered. The approach presented makes use of the bumpless transfer technique and gives a switching performance optimal controller design method for coping with bumps and undesirable transients in multiplemode switching systems. Simulation results for the generic hypersonic vehicle model show the effectiveness of the proposed design method.

作者: Yiwen Qi Wen Bao

作者单位: Hypersonic Technology Research Center,Harbin Institute of Technology,150010 Harbin,China.

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 140-145

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）