DOI: https://doi.org/10.18524/1810-4215.2014.27.82632

THE SIMULATION OF THE ORBITAL EVOLUTION OF A PASSIVE HIGH-ORBIT FRAGMENT WITH LARGE SURFACE AREA

A. A. Bazyey

Анотація


The numerical integration of the motion equations of a passive high-orbit fragment with large surface area was performed accounting for the main gravitational perturbations of the Earth, Moon and Sun, as well as the solar radiation pressure. Based on the numerical model of motion in the near-Earth space that accounts for only the most powerful perturbations, a new method for de-orbiting artificial celestial bodies from high altitudes is suggested.


Ключові слова


methods: numerical–celestialme-chanics

Повний текст:

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Посилання


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Volvach A.E., Roumyantsev V.V., MolotovI.E. et al.: 2006, Space Science and Technology, 12, No.5/6, 50.




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