Research of Trajectory Tracking Control of Cruise Missile Based on Observer

摘要：

　　To achieve cruise missile accurate trajectory tracking control,an observer-based tracking control method is designed.An observer is developed to estimate the states and control signals of desired trajectory as the inputs of the tracking controller.The linear quadratic optimal control is used to realize full-state feedback control for trajectory tracking.A certain cruise missile is used for the tracking simulation and the result shows satisfactory performance,the control method is simple and suitable for engineering applications.

关键词： Cruise missile Observer Trajectory tracking Quadratic optimal control

作者: Bo Hao Fan Li Jianhui Zhao

作者单位: School of Instrument Science and Optical-Electronics Engineering,Beijing University of Aeronautics and Astronautics, Beijing 100191, China

会议类型: 国际会议

会议名称: the 2012 International Conference on Frontiers of Mechanical Engineering and Materials Engineering (机械工程与材料工程国际会议())

会议地点: 香港

会议语种:英文

页码: 1599-1602

在线出版日期: 2012-07-27（万方平台首次上网日期，不代表论文的发表时间）