Finite-time Convergent Guidance and Control Based on Integrated Model

摘要：

　　An integrated guidance and control model for missile control system design is established in this paper.Finite-time stability theory is used to design a finite-time convergent guidance and control law based on the proposed model.Some simulation tests are done to verify the validity of the control law designed in this paper and the advantages compared with other guidance laws.The results show the control designed in this paper can satisfy the terminal indicators accurately.

关键词： finite-time convergence control the integrated model terminal guidance

作者: Lin Lin Songyan Wang Tao Chao Ming Yang

作者单位: Control and Simulation Center,Harbin Institute of Technology,Harbin 150001,China

会议类型: 国际会议

会议名称: 第26届中国控制与决策会议(2014 CCDC)

会议地点: 长沙

会议语种:英文

页码: 676-680

在线出版日期: 2014-05-31（万方平台首次上网日期，不代表论文的发表时间）