INVESTIGATION ON EJECTION DYNAMICS OF AIR LAUNCHED MISSILE

摘要：

An air launched missile and its ejection type launcher was modeled to investigate their performance. The launcher used a pneumatic system with high pressure cylinder as power source. Based on the mathematical models of the pneumatic elements, a model for the pneumatic system of the launcher was developed using MATLAB/Simulink. Blocks of condition selection and judgment were adopted in Simulink to simulate the separation between the missile and the pneumatic actuator of the launcher. The missile was modeled as a rigid body and a flexible body in the software ADAMS. The dynamic response of the missile and the performance of the pneumatic system were obtained by conducting co-simulation. The difference between the results of the rigid body and flexible body model for the missile is small. It is showed that the rigid body assumption for the missile is acceptable to investigate the ejection dynamics.

关键词： air launched missile ejection dynamics pneumatic multi-body dynamics co-simulation

作者: B.Xu G.Liu J.D.Yang W.Zhang

作者单位: Department of Mechanics and Engineering Science, Fudan University, Shanghai 200433, China The 8th In The 8th Institute of Shang Academy of Spaceflight Technology, Shanghai 200233, China Department of Mechanics and Engineering Science, Fudan University, Shanghai 200433, China

会议类型: 国际会议

会议名称: 2012 International Conference on System Simulation(2012年国际系统仿真学术会议)

会议地点: 上海

会议语种:英文

页码: 5-10

在线出版日期: 2012-04-06（万方平台首次上网日期，不代表论文的发表时间）