Abstract
A highly accurate algorithm for synthesizing chains of cranking gravity-assist maneuvers (GAMs) has been constructed using formalization of the search for ballistic scenarios followed by the adaptive involvement of tens of millions of variants. Its use results in a significant change in the orbital inclination of a research spacecraft without a significant expenditure of propellant with a reasonable mission time.
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Original Russian Text © Yu.F. Golubev, A.V. Grushevskii, V.V. Koryanov, A.G. Tuchin, D.A. Tuchin, 2017, published in Doklady Akademii Nauk, 2017, Vol. 472, No. 4, pp. 403–406.
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Golubev, Y.F., Grushevskii, A.V., Koryanov, V.V. et al. A technique for designing highly inclined spacecraft orbits using gravity-assist maneuvers. Dokl. Phys. 62, 76–79 (2017). https://doi.org/10.1134/S1028335817020033
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DOI: https://doi.org/10.1134/S1028335817020033