Trajectory deflection correction by miniature pulse thruster groups is an efficiency method of improving rocket projectile firing precision and reducing the scattering of impact point.
采用小型脉冲推力器组修正弹道偏差是提高火箭弹射击精度，减小落点散布的有效方法。
As an example, the paper then describes a newly developed light pulse irradiant uniformity measurement system and the correction method for its measurement result.
以闪光光强分布的均匀性测量为例，介绍了太阳电池电性能测量光照均匀性瞬态测量系统及其修正方法。
Based on the principle on parabolic and proportional navigation guidance (PAPNG), the required pulse number for trajectory correction was analyzed in detail.
基于抛物线比例导引原理，详细分析了弹道修正所需求的脉冲数。
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