One State-unmeasured Missile Control System Design

摘要：

The pitch channel output tracking of a kind of supersonic cruise missile over-load control system was designed based on second order sliding mode control theory. Output-redefinition approach was adopted to resolve the non-minimum phase problem between rudder angle and overload output of STT missile system, second order sliding mode control was used to eliminate chatter, and guaranteed the tracing of original system output. The observer was designed to deal with the not complete state measurable system. The stability and robustness were verified by the simulations results.

关键词： Observer Non-minimum phase Zero dynamic Output-redefinition Second order sliding mode

作者: Chen Jie Wu Jinhua Pan Changpeng

作者单位: Department of Control Engineering, Naval Aeronautical and Astronautical University, Yantai, 264001, Department of Command, Naval Aeronautical and Astronautical University, Yantai, 264001, China

会议类型: 国际会议

会议名称: 2009年中国控制与决策会议(2009 Chinese Control and Decision Conference)

会议地点: 广西桂林

会议语种:英文

页码: 441-444

在线出版日期: 2009-06-17（万方平台首次上网日期，不代表论文的发表时间）