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论述了根据弹上纵向加速度计的响应估算导弹发动机推力曲线的近似方法。最后,通过计算分析了该方法所能达到的精度。
The approximate method of estimating the thrust curve of a missile engine based on the response of the longitudinal accelerometer on the projectile is discussed. Finally, the precision that this method can achieve is analyzed through calculation.