Partial Integrated Missile Guidance and Control with Output Feedback

摘要：

　　A novel output feedback controller is presented in this paper for a class of nonlinear systems with disturbances.Firstly,a dynamic compensator is introduced and combined with the plant to form an extended system for which an estimator is constructed.Using the norm bound of estimation error vector,the controller is proposed to drive the output to zero in finite time.Then the proposed result is applied to partial integrated guidance and control design of missile to achieve hit-to-kill interception.Finally,a simulation example is presented to illustrate effectiveness of the proposed method.

关键词： Output feedback Observer Finite time Integrated guidance and control

作者: Xianghua Wang Jinzhi Wang Gang Gao

作者单位: 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 33th Chinese Control Conference第33届中国控制会议

会议地点: 南京

会议语种:英文

页码: 713-718

在线出版日期: 2014-07-28（万方平台首次上网日期，不代表论文的发表时间）