Static Output Feedback For Aeroengine Control System

摘要：

This paper considers the static output feedback control synthesis problem of aeroengine system. By introducing a slack variable for separating system matrix and Lyapunov matrix, more relaxed sufflcient conditions for designing static output feedback controller are given in terms of solutions to a set of linear matrix inequalities. Simulation illustrates that the proposed methods for aeroengine systems can achieve good performance.

关键词： SISO control multivariable control linear matrix inequalities robust H2 control static output feedback aeroengine.

作者: Binbin Hao Tao Qu

作者单位: AVIC shenyang engine design andresearch institute, Shenyang, 110015, China. AVIC shenyang engine design and research institute, Shenyang, 110015, China.

会议类型: 国际会议

会议名称: The 24th Chinese Control and Decision Conference (第24届中国控制与决策学术年会 2012 CCDC)

会议地点: 太原

会议语种:英文

页码: 4250-4253

在线出版日期: 2012-05-23（万方平台首次上网日期，不代表论文的发表时间）