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• W2963415603 abstract "We develop a computational approach for the design of continuous low thrust transfers in the planar circular restricted three-body problem. The use of low thrust propulsion allows the spacecraft to depart from the natural dynamics and enables a wider range of transfers. We generate the reachable set of the spacecraft and use this to determine transfer opportunities, analogous to the intersection of control-free invariant manifolds. The reachable set is developed on a lower dimensional Poincaré section and used to design transfer trajectories. This is solved numerically as a discrete optimal control problem using a variational integrator, which preserves the geometric structure of the motion in the three-body problem. We demonstrate our approach with two numerical simulations of transfers in the Earth-Moon three-body system." @default.
• W2963415603 created "2019-07-30" @default.
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• W2963415603 date "2019-01-09" @default.
• W2963415603 modified "2023-09-23" @default.
• W2963415603 title "Systematic Design of Optimal Low-Thrust Transfers for the Three-Body Problem" @default.
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• W2963415603 doi "https://doi.org/10.1007/s40295-018-00139-y" @default.
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