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介绍了牛顿—欧拉法及第一类拉格朗日方程法在火箭武器系统发射动力学仿真方面的应用，并对两种方法的仿真结果进行了对比分析。
The application of Newton - Euler method and Lagrange equation of the first kind in the launch vehicle dynamics simulation of rocket weapon system is introduced. The simulation results of the two methods are compared and analyzed.