提出了一种基于空中发射点的在线诸元计算方法，该方法具有计算量小、制导方法误差小的特点，可用于陆基机动弹道导弹或潜射弹道导弹的快速发射。
The method has minor computer load and small guidance method error; therefore it can be used in rapid launching of land-based maneuver ballistic missiles or.
提出了一种基于空中发射点的在线诸元计算方法，该方法具有计算量小、制导方法误差小的特点，可用于陆基机动弹道导弹或潜射弹道导弹的快速发射。
The method has minor computer load and small guidance method error; therefore it can be used in rapid launching of land-based maneuver ballistic missiles or.
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