为火箭助飞鱼雷的弹道仿真研究提供有效的平台,根据火箭助飞鱼雷全弹道运动流程,建立了其空中和水下的动力学、运动学、控制导引及风场环境等模型,应用面向对象方法设计了仿真模型,构建了仿真系统。对典型态势进行仿真,得到了全弹道曲线和特征点处战技指标参数,结果表明所建模型正确,仿真系统具有良好的可操作性。

In order to provide an effective test bed for the rocket-assisted torpedo trajectory simulation research, according to the motion process of its trajectories, the models of the dynamics, the kinematical equation, the guidance and control equation, the wind field environment, etc. in air and under the water were built, and the object-oriented methods were applied to the simulation system design. The trajectory curves and technical parameters of characteristic points were acquired. The results show that the models are reliable, and the simulation system is exercisable.