standard reentry trajectory

In transition phase followed braking phase, a standard reentry trajectory is computed and stored using landing point prediction guidance method ( LPPGM).

该方法融合了落点预报制导方法和基准弹道制导方法的长处。

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The present paper discusses the adjustable ability and design method of a standard spacecraft reentry trajectory.

本文研究载人飞船三自由度标准返回轨道的设计方法.

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Task of designing reentry trajectory of manned spacecraft is to make standard reentry trajectory and laws of guidance and control according to requirement of task.

载人飞船返回再入轨道设计的主要任务是确定出标准返回轨道和再入制导规律。

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