Pole Assignment Method with State Constraints for Missile Three-loop Autopilot Design

摘要：

The three-loop autopilot is transformed into states space model, and the feasibility of presupposition of some nuisance parameter is proved. A new pole assignment method is studied. Considering the actuator state feedback constraints, search methods are used to find the additional poles introduced by actuator. The design results show that, with the new method, all the poles of the system can be assigned to the desired place.

关键词： three-loop autopilot pole assignment state feedback constraints

作者: CHANG Chao LIN De-fu WANG Jiang

作者单位: School of Aerospace Science and Engineering, Beijing Institute of Technology, Beijing 100081

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: 3298-3301

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）