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首页> 外文期刊>Journal of guidance, control, and dynamics >Survey of Highly-Non-Keplerian Orbits with Low-Thrust Propulsion
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Survey of Highly-Non-Keplerian Orbits with Low-Thrust Propulsion

机译：低推力高非克里普勒轨道的调查

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摘要

As has been demonstrated, using continuous-low-thrust propulsion to enable highly-non-Keplerian orbits (termed such when the magnitude of the acceleration applied is of approximately equal magnitude to that of the gravitational acceleration experienced) is a rich vein of astrodynamics research, both currently and in broader historical terms. It has been shown here that the problem has been considered from a number of different viewpoints, in terms of propulsion systems [e.g., solar electric propulsion (SEP), solar sails, hybrid SEP/sail, and other more exotic methods] and considerations of the iV-body problem (e.g., two-body, three-body circular restricted and elliptical restricted, and four-body restricted). Many authors have analyzed the dynamics, stability, and control of such orbits and determined orbits that connect them with other orbits, both Keplerian and non-Keplerian.
机译：如已证明的那样，使用连续低推力推进来实现高度非克里普勒轨道（当所施加的加速度的大小与所经历的重力加速度的大小大致相等时，则被称为），这是航天动力学研究的重要内容，无论是当前还是更广泛的历史术语而言。此处已表明，从推进系统（例如，太阳能电动推进（SEP），太阳帆，混合式SEP /帆和其他更奇特的方法）和对iV体问题（例如，两体，三体圆形限制和椭圆体限制，以及四体限制）。许多作者分析了此类轨道的动力学，稳定性和控制性，并确定了将它们与开普勒和非开普勒轨道连接起来的轨道。

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