建立了采用脉冲力控制的弹道修正弹飞行弹道模型。
The trajectory correction projectile model using impulse was established.
在常用坐标系下，推导了空间运动的数学模型，设计了方案飞行弹道。
Under the usual coordinates, the paper conclude mathematical model in space motion and design project ballistic trajectory.
修正过程中首先要采用某种测试手段在飞行弹道上逐点进行诸元测量。
A kind of measurement would be used to measure ballistic parameters on different points of trajectory for this correction.
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