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Journal of Automation and Information Sciences
SJR: 0.275 SNIP: 0.59 CiteScore™: 0.8

ISSN Imprimir: 1064-2315
ISSN On-line: 2163-9337

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Journal of Automation and Information Sciences

DOI: 10.1615/JAutomatInfScien.v35.i8.30
13 pages

Use of Equinoctial Orbital Elements as Variables in the Problem of Minimal Time Orbit-to-Orbit Transfer in Strong Gravitational Field under Fixed-Value Thrust

Boris N. Kiforenko
S.P. Timoshenko Istitute of Mechanics of National Academy of Sciences of Ukraine, Kiev, Ukraine
Zoya V. Pasechnik
Kyiv National Taras Shevchenko University, Kyiv, Ukraine
Igor Yu. Vasil'ev
Kyiv National Taras Shevchenko University, Kyiv, Ukraine


A problem of minimal time transfer between elliptic orbits of a spacecraft (SC) with a small constant magnitude and regulated direction thrust in a central gravitational field is considered. Unlike earlier papers [1, 2], for obtaining averaged equations of optimal motion, in this work the authors used a system of equinoctial orbital elements. This technique enables one to eliminate singularities associated with zero values of either eccentricity or inclination of elliptic orbit in equations of motion.

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