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Spacecraft reentry trajectory optimization is a kind of optimal control problem.
飞行器再入轨迹优化是一类最优控制问题.
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The flight laws, characteristics and point precision of spiral reentry trajectory were studied by simulating calculation.
通过仿真计算,研究了螺旋再入弹道的飞行规律 、 特点以及落点精度等问题.
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.
再入轨道???
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