Based on the practice in ballistic correction, the paper carried through gyroscope's system analysis and design.
论文基天弹道修正的实际应用，对微陀螺进行了系统分析与设计，主要完成了以下几方面的工作。
The model can be applied further to ballistic correction, parameter optimization and ballistic simulation of TSP systems.
该模型可进一步用于末敏弹系统的弹道修正、参数优化和弹道模拟。
A kind of measurement would be used to measure ballistic parameters on different points of trajectory for this correction.
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。
Based on theory of exterior ballistic and impulse motor, the ballistic model is set up to simulate the trajectory correction projectile with impulse and impulse moments.
该文对弹道修正技术中常采用的脉冲力矩修正作用 ，对弹丸飞行稳定性状况的影响等进行了讨论 ，给出了脉冲力矩作用下飞行稳定性条件。
Different drag correction coefficients at different time points are introduced, and then both speed curve and ballistic curve fitting are finished.
采用在不同时间点增加阻力系数修正系数的方法拟合速度-时间曲线和位置-时间曲线。
Different drag correction coefficients at different time points are introduced, and then both speed curve and ballistic curve fitting are finished.
采用在不同时间点增加阻力系数修正系数的方法拟合速度-时间曲线和位置-时间曲线。
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