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

ISSN Imprimir: 1064-2315
ISSN En Línea: 2163-9337

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Journal of Automation and Information Sciences

DOI: 10.1615/JAutomatInfScien.v35.i12.30
12 pages

The Problem of Determination of Solutions of Motion Equations of Spacecraft with Low Thrust on Trajectories Close to Optimal, Obtained by the Averaging Method

Boris N. Kiforenko
S.P. Timoshenko Istitute of Mechanics of National Academy of Sciences of Ukraine, Kiev, Ukraine
Sergey V. Vasilenko
Kyiv National Taras Shevchenko University, Ukraine
Zoya V. Pasechnik
Kyiv National Taras Shevchenko University, Kyiv, Ukraine

SINOPSIS

We investigate the problem of construction of exact numerical solutions of motion equations of a spacecraft with low thrust engine, which realizes transfer between distant orbits in the Newton central gravity field. Approximate solution of the classical problem of mechanics of space flight about transfer with maximal payload under given launching mass is constructed by the averaging method. We discussed variants of determination of solutions of exact motion equations on trajectories, which move away not too much from the trajectory of the averaged solution. One of the suggested variants is shown for example of interorbital transfer with simultaneous changing of the major semiaxis, eccentricity and angle of orbit inclination.


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