CAMELOT - computational-analytical multi-fidelity low-thrust optimisation toolbox
Di Carlo, Marilena and Romero Martin, Juan Manuel and Vasile, Massimiliano; (2016) CAMELOT - computational-analytical multi-fidelity low-thrust optimisation toolbox. In: 6th International Conference on Astrodynamics Tools and Techniques (ICATT). ESA, DEU.
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Abstract
CAMELOT (Computational-Analytical Multi-fidelity Low-thrust Optimisation Toolbox) 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. In order 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 by using two pptimisation engines included in the toolbox, a single objective global optimiser and a combinatorial optimisation algorithm. CAMELOT has been applied to a variety of applications: from the design of interplanetary trajectories to the optimal deorbiting of space debris, from the deployment of constellations to on-orbit servicing. In this paper the main elements of CAMELOT are described and two space mission design problems solved using the toolbox are described.
Creators(s): |
Di Carlo, Marilena ![]() ![]() ![]() | Item type: | Book Section |
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ID code: | 59513 |
Keywords: | multi-target missions, surrogate models, multi-fidelity, combinatorial problems, low-thrust propulsion, Motor vehicles. Aeronautics. Astronautics, Aerospace Engineering |
Subjects: | Technology > Motor vehicles. Aeronautics. Astronautics |
Department: | Faculty of Engineering > Mechanical and Aerospace Engineering Technology and Innovation Centre > Advanced Engineering and Manufacturing |
Depositing user: | Pure Administrator |
Date deposited: | 20 Jan 2017 12:01 |
Last modified: | 08 Jan 2021 01:58 |
Related URLs: | |
URI: | https://strathprints.strath.ac.uk/id/eprint/59513 |
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