Modeling and Simulation of External Ballistics of New Air-Defence Guided Projectile

Yao Hong-He, Lu Fa-xing
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Abstract

The method of three-dimensional ballistic modeling and simulation of shipborne air-defence guided projectile is discussed. Firstly, the force and guidance law of the projectile are analyzed, and taking the proportional guidance as an example, the method establish the simulation model of the air-defence guided projectile ballistic from the perspective by dynamics. Secondly, the selection criteria of some parameters are discussed, and the three-dimensional ballistic simulation is performed by Matlab. Finally, the effects of the motion parameters such as projectile speed, target speed and proportional coefficient on the trajectory and encounter time are analyzed. The simulation results show that the method is correct and feasible, and it has certain significance for the ballistic design and optimization of shipborne air-defence guided projectile.
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新型防空制导弹外弹道建模与仿真
讨论了舰载防空制导弹的三维弹道建模与仿真方法。首先,分析了弹丸的受力和制导规律,并以比例制导为例,从动力学角度建立了防空制导弹丸弹道仿真模型。其次,讨论了部分参数的选择准则,并利用Matlab进行了三维弹道仿真。最后,分析了弹丸速度、目标速度和比例系数等运动参数对弹道和相遇时间的影响。仿真结果表明,该方法是正确可行的,对舰载防空制导弹的弹道设计与优化具有一定的指导意义。
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