Research on Launch Dynamics Modeling and Simulating for Surface-to-air Missile Supported by Adapter

摘要：

　　The launch dynamics analysis model of surface-to-air missile supported by the adapter was established,and the model was verified by test data.Simulation analysis shows: the missile begins to generate pitch angular speed at semi-constrained state after mid-adapter leave the tube,and the speed increases with distance between the mid-adapter and the rear adapter,and as the thrust of the engine increases to decreases,as the launch angle decreases,the missiles pitch angular speed increases,gravity is the main cause of the launch disturbance in the direction of the pitching.

作者: Liu Chaoqi Wen LiHua He Jiangjun Liu Yuxiang

作者单位: Northwestern Polytechnical University,Xian 710072,China;Jiangnan Institute of Electromechanical sys Northwestern Polytechnical University,Xian 710072,China Jiangnan Institute of Electromechanical system design,Guiyang 55009,China

会议类型: 国际会议

会议名称: 2018年建筑、航空与环境工程国际学术论坛-物联网(IFCAE-IOT 2018)2018 International Forum on Construction, Aviation and Environmental Engineering-Internet of Things(IFCAE-IOT 2018)

会议地点: 广州

会议语种:英文

页码: 1-5

在线出版日期: 2018-05-11（万方平台首次上网日期，不代表论文的发表时间）