Optimization of Interplanetary Trajectories Using the Colliding Bodies Optimization Algorithm
In this paper, a recent physics-based metaheuristic algorithm, the Colliding Bodies Optimization (CBO), already employed to solve problems in civil and mechanical engineering, is proposed for the optimization of interplanetary trajectories by using both indirect and direct approaches. The CBO has an...
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| Format: | Article |
| Language: | English |
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Wiley
2020-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2020/9437378 |
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| _version_ | 1849683249247289344 |
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| author | Marco Del Monte Raffaele Meles Christian Circi |
| author_facet | Marco Del Monte Raffaele Meles Christian Circi |
| author_sort | Marco Del Monte |
| collection | DOAJ |
| description | In this paper, a recent physics-based metaheuristic algorithm, the Colliding Bodies Optimization (CBO), already employed to solve problems in civil and mechanical engineering, is proposed for the optimization of interplanetary trajectories by using both indirect and direct approaches. The CBO has an extremely simple formulation and does not depend on any initial conditions. To test the performances of the algorithm, missions with remarkably different orbital transfer energies are considered: from the simple planar case, as the Earth-Mars orbital transfer, to more energetic ones, like a rendezvous with the asteroid Pallas. |
| format | Article |
| id | doaj-art-dbf36ca2ffb243c3be43dc837a7e6f3b |
| institution | DOAJ |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2020-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-dbf36ca2ffb243c3be43dc837a7e6f3b2025-08-20T03:23:57ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742020-01-01202010.1155/2020/94373789437378Optimization of Interplanetary Trajectories Using the Colliding Bodies Optimization AlgorithmMarco Del Monte0Raffaele Meles1Christian Circi2Department of Astronautical, Electrical and Energy Engineering, Sapienza University of Rome, Via Salaria 851, 00138 Rome, ItalyDepartment of Astronautical, Electrical and Energy Engineering, Sapienza University of Rome, Via Salaria 851, 00138 Rome, ItalyDepartment of Astronautical, Electrical and Energy Engineering, Sapienza University of Rome, Via Salaria 851, 00138 Rome, ItalyIn this paper, a recent physics-based metaheuristic algorithm, the Colliding Bodies Optimization (CBO), already employed to solve problems in civil and mechanical engineering, is proposed for the optimization of interplanetary trajectories by using both indirect and direct approaches. The CBO has an extremely simple formulation and does not depend on any initial conditions. To test the performances of the algorithm, missions with remarkably different orbital transfer energies are considered: from the simple planar case, as the Earth-Mars orbital transfer, to more energetic ones, like a rendezvous with the asteroid Pallas.http://dx.doi.org/10.1155/2020/9437378 |
| spellingShingle | Marco Del Monte Raffaele Meles Christian Circi Optimization of Interplanetary Trajectories Using the Colliding Bodies Optimization Algorithm International Journal of Aerospace Engineering |
| title | Optimization of Interplanetary Trajectories Using the Colliding Bodies Optimization Algorithm |
| title_full | Optimization of Interplanetary Trajectories Using the Colliding Bodies Optimization Algorithm |
| title_fullStr | Optimization of Interplanetary Trajectories Using the Colliding Bodies Optimization Algorithm |
| title_full_unstemmed | Optimization of Interplanetary Trajectories Using the Colliding Bodies Optimization Algorithm |
| title_short | Optimization of Interplanetary Trajectories Using the Colliding Bodies Optimization Algorithm |
| title_sort | optimization of interplanetary trajectories using the colliding bodies optimization algorithm |
| url | http://dx.doi.org/10.1155/2020/9437378 |
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