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Simulation and experimental research on line throwing rocket with flight 被引量:2
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作者 Wen-bin GU Ming LU +3 位作者 Jian-qing LIU Qin-xing DONG Zhen-xiong WANG Jiang-hai CHEN 《Defence Technology(防务技术)》 SCIE EI CAS 2014年第2期149-153,共5页
The finite segment method is used to model the line throwing rocket system.A dynamic model of line throwing rocket with flight motion based on Kane's method is presented by the kinematics description of the system... The finite segment method is used to model the line throwing rocket system.A dynamic model of line throwing rocket with flight motion based on Kane's method is presented by the kinematics description of the system and the consideration of the forces acting on the system.The experiment designed according to the parameters of the dynamic model is made.The simulation and experiment results,such as range,velocity and flight time,are compared and analyzed.The simulation results are basically agreed with the test data,which shows that the flight motion of the line throwing rocket can be predicted by the dynamic model.A theoretical model and guide for the further research on the disturbance of rope and the guidance,flight control of line throwing rocket are provided by the dynamic modeling. 展开更多
关键词 火箭系统 飞行运动 实验 仿真 动态模型 有限段方法 参数设计 飞行时间
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