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EnglishThis paper analyzes the locally-optimal heliocentric transfer of a spacecraft propelled by an Electric Solar Wind Sail, an innovative propellantless propulsion system that generates a propulsive acceleration exploiting the momentum of solar wind particles. The potentialities of such an advanced thruster are investigated in terms of flight times required to achieve a given heliocentric orbit. The problem is addressed using a locally optimal formulation, by minimizing a scalar performance index that depends on the time derivatives of the osculating orbital elements. The proposed algorithm gives an estimate of the globally optimal flight time with reduced computational efforts compared to a traditional optimization approach. Also, when the performance index involves a single orbital parameter and the transfer trajectory is two-dimensional, the proposed approach provides an analytical solution to the locally-optimal control problem. The procedure discussed in the paper is used to quantify the near-optimal performance of an Electric SolarWind Sail in some advanced mission scenarios, such as the design of a heliocentric non-Keplerian orbit for solar activity monitoring, the exploration of the Solar System boundaries, and the rendezvous with comets 1P Halley and 67P/Churyumov-Gerasimenko.
| Autori interni: | BASSETTO, MARCO (Primo) QUARTA, ALESSANDRO ANTONIO (Secondo) MENGALI, GIOVANNI (Ultimo) | |
| Autori: | Bassetto, Marco; Quarta, ALESSANDRO ANTONIO; Mengali, Giovanni | |
| Titolo: | Locally-Optimal Electric Sail Transfer | |
| Anno del prodotto: | 2019 | |
| Abstract: | This paper analyzes the locally-optimal heliocentric transfer of a spacecraft propelled by an Electric Solar Wind Sail, an innovative propellantless propulsion system that generates a propulsive acceleration exploiting the momentum of solar wind particles. The potentialities of such an advanced thruster are investigated in terms of flight times required to achieve a given heliocentric orbit. The problem is addressed using a locally optimal formulation, by minimizing a scalar performance index that depends on the time derivatives of the osculating orbital elements. The proposed algorithm gives an estimate of the globally optimal flight time with reduced computational efforts compared to a traditional optimization approach. Also, when the performance index involves a single orbital parameter and the transfer trajectory is two-dimensional, the proposed approach provides an analytical solution to the locally-optimal control problem. The procedure discussed in the paper is used to quantify the near-optimal performance of an Electric SolarWind Sail in some advanced mission scenarios, such as the design of a heliocentric non-Keplerian orbit for solar activity monitoring, the exploration of the Solar System boundaries, and the rendezvous with comets 1P Halley and 67P/Churyumov-Gerasimenko. | |
| Digital Object Identifier (DOI): | 10.1177/0954410017728975 | |
| Appare nelle tipologie: | 1.1 Articolo in rivista |
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