结果表明，在发动机点火时间范围内，点火时间对无控弹道射程和惯性制导启控点散布影响不大。
Results show that the rocket ignition time has little effect on uncontrolled trajectory and the dispersion of the starting position of guidance in the range of the rocket ignition time.
采用姿态稳定技术后远程火箭弹的横向散布得到有效改善，但纵向散布仍然较大，需要进一步对射程进行修正。
Although attitude stabilization technology reduces the lateral dispersion of long-range rockets effectively, their range dispersion is still not satisfactory.
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