计算结果表明，使用经各种误差修正后的测速数据参与初轨计算能有效提高定轨精度。
The result shows that using velocity measuring data after error correction in preliminary orbiting computation can effectively improve the orbit determination precision.
提出了一种基于误差知识的二重插值DFT方法用于高精度时钟初相测量。
A high performance measurement of initial phase via a Dual Interpolated DFT method based on error information is presented.
该初制导方法能补偿制导方法误差和轨道摄动对拦截脱靶量的影响。
The miss distance caused by guidance method error and the effects of perturbation are compensated in this initial guidance law.
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