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- W3100653013 abstract "In this paper, we present the controllability properties of Keplerian motion controlled by low-thrust control systems. A low-thrust control system, compared with a high or an even impulsive control system, provides a fuel-efficient means to control the Keplerianmotion of a satellite in the restricted two-body problem.We obtain that, for any positive value of maximum thrust, the motion is controllable for orbital transfer problems. For two other typical problems-de-orbit problem and orbital insertion problem, which have state constraints - the motion is controllable if and only if the maximum thrust is bigger than a limiting value. Finally, two numerical examples are given to show the numerical method to compute the limiting value." @default.
- W3100653013 created "2020-11-23" @default.
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- W3100653013 date "2016-12-19" @default.
- W3100653013 modified "2023-09-25" @default.
- W3100653013 title "11. Controllability of Keplerian motion with low-thrust control systems" @default.
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- W3100653013 doi "https://doi.org/10.1515/9783110430394-011" @default.
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