A two-step LMI approach to robust dynamic output feedback control for the MIMO aircraft model F-18

摘要：

This work is concerned with robust dynamic output feedback controller design for a simplified aircraft model F-18 which can be rewritten as a LPV system. A general LMI-based two-step approach is proposed to tackle this problem. Such a separation procedure overcomes the limitation of traditional approach that can not be applied to the linear parameter varying (LPV) system. Numerical results show the proposed controller can ensure simultaneous quadratic stability with H1 performance and satisfactory dynamic performance for a selected flight envelop containing some operating points.

作者: Lei Song Jianying Yang

作者单位: State Key Lab for Turbulence and Complex Systems and Department of Mechanics and Aerospace Engineering,College of Engineering,Peking University,Beijing 100871,P.R.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: 76-81

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）