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- W2590491558 abstract "Computational-Analytical Multi-fidElity Low-thrust Optimisation Toolbox (CAMELOT) is a toolbox for the fast preliminary design and optimisation of low-thrust trajectories. It solves highly complex combinatorial problems to plan multi-target missions characterised by long spirals including different perturbations. To do so, CAMELOT implements a novel multi-fidelity approach combining analytical surrogate modelling and accurate computational estimations of the mission cost. Decisions are then made using two optimisation engines included in the toolbox, a single-objective global optimiser, and a combinatorial optimisation algorithm. CAMELOT has been applied to a variety of case studies: from the design of interplanetary trajectories to the optimal de-orbiting of space debris and from the deployment of constellations to on-orbit servicing. In this paper, the main elements of CAMELOT are described and two examples, solved using the toolbox, are presented." @default.
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- W2590491558 date "2017-09-22" @default.
- W2590491558 modified "2023-10-18" @default.
- W2590491558 title "CAMELOT: Computational-Analytical Multi-fidElity Low-thrust Optimisation Toolbox" @default.
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- W2590491558 doi "https://doi.org/10.1007/s12567-017-0172-6" @default.
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