Recent years, Rendezvous and Docking, space attack and defense, space detection is the focus of astronautics research. It results in space vehicle doing long-time and extensive orbit transfer.
近年来,交会对接、空间攻防、星际探测成为航天研究的热点,长时间、大范围的轨道机动成为必然。
参考来源 - 轨道机动航天器的SINS/GPS组合导航系统算法研究This paper investigates problems of optimum orbit transfer and rendezvous.
本文研究航天器轨道转移与轨道交会的最优控制问题。
参考来源 - 航天器轨道转移与交会最优控制研究·2,447,543篇论文数据，部分数据来源于NoteExpress
In this case, the study of orbit transfer insertion error becomes very complicated.
在这种情况下，轨道转移入轨误差的研究变得较为复杂。
In this paper, thinking of three-satellite constellation, optimal impulse orbit transfer is studied for constellation launching.
文中基于卫星相对运动状态转移方程，推出了星座双脉冲式变轨控制的理论解；
In this paper, thinking of small satellite constellation, optimal impulse orbit transfer is studied for constellation launching.
针对小卫星星座，进行星座发射中的最优脉冲式变轨研究。
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