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.
Optimization of interplanetary trajectories using the colliding bodies optimization algorithm / Del Monte, Marco; Meles, Raffaele; Circi, Christian. - In: INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING (ONLINE). - ISSN 1687-5974. - (2020), pp. 1-17. [10.1155/2020/9437378]
Optimization of interplanetary trajectories using the colliding bodies optimization algorithm
Christian Circi
2020
Abstract
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.File | Dimensione | Formato | |
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