Agile Turn Control for Air-to-Air Missile Based on Reaction Jet Control System

摘要：

　　This paper focuses on agile turn control for air-to-air missile flying in the horizontal plane.The attitude dynamics is discussed and variable structure control (VSC) method for attitude control is analyzed.After analysis of the dynamic function about velocity angle,a staged control method using VSC based on reaction jet control system (RCS) is proposed to achieve fast change of velocity direction and attitude in a short time.The simplex method is used for trajectory optimization.The simulation results show the feasibility of the staged control method which makes the missile turn faster than the situation of attitude control method.The new method demonstrates that RCS is able to control the missile to realize 180°change both for the velocity angle and attitude angle.

关键词： Air-to-air missile Reaction jet control system Variable structure control Simplex method

作者: Yue Yue Ma Sheng Jing Tang

作者单位: Key Laboratory of Dynamics and Control of Flight Vehicle,Ministry of Education,Beijing Institute of Technology,Beijing,100081,China

会议类型: 国际会议

会议名称: the 2012 International Conference on Manufacturing Engineering and Automation (2012年制造工程与自动化国际会议(ICMEA2012))

会议地点: 广州

会议语种:英文

页码: 1285-1288

在线出版日期: 2012-11-16（万方平台首次上网日期，不代表论文的发表时间）