THE ORBITS DISIGNING FOR INTERPLANETARY PROBES AND ARTIFICIAL PLANETARY SATELLITES
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摘要: 本文探讨行星际探测器和人造行星卫星的动力学模型,研究它们的运动轨道,给出飞行时间的近似式,并且从飞行时间和消耗能量二个方面对它们的轨道设计问题提出了一些新的看法.另外,文中还讨论了人造行星卫星的运动及其稳定条件.Abstract: In this paper, the dynamical model, orbital motion and mission time for interplanetary probe and artificial planetary satellite are given. The disign for orbit to cut mission time and save fuel is discussed and the stable region of artificial planetary satellite is also obtained.
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