DETERMINATION OF POLE AND ROTATION PERIOD OF NOT STABILIZED ARTIFICIAL SATELLITE BY USE OF MODEL

Автор(и)

  • S. Ya. Kolesnik Department of Astronomy, Odessa State University T.G.Shevchenko Park, Odessa 65014 Ukraine, Ukraine
  • A. V. Dobrovolsky Department of Astronomy, Odessa State University T.G.Shevchenko Park, Odessa 65014 Ukraine, Ukraine
  • N. G. Paltsev Department of Astronomy, Odessa State University T.G.Shevchenko Park, Odessa 65014 Ukraine, Ukraine

DOI:

https://doi.org/10.18524/1810-4215.2004.17.93214

Анотація

The algorithm of determination of orientation of rotation axis (pole) and rotation period of satellite, simulated by a cylinder, which is precessing around of vector of angular moment of pulse with constant nutation angle is offered. The Lambert's law of light reflection is accepted. Simultaneously, dependence of light reflection coefficient versus phase angle is determined. The model's simulation confirm applicability of this method. Results of the calculations for artificial satellite No 28506 are carried out.

Посилання

Grigorevsky V.M., Zgonjajko N.S., Kolesnik S.Ya.: 1979, Pis'ma A.Zh., 5, No 9, 482.

McCue G.A., Williams J.G., Morford J.M.: 1971, Planetary and Space Science, 19, 851.

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Опубліковано

2017-03-15

Номер

Том 17 (2004)

Розділ

Статті

Ліцензія

Авторське право (c) 2017 Odessa Astronomical Publications

Creative Commons License

Ця робота ліцензується відповідно до Creative Commons Attribution-NonCommercial 4.0 International License.

Відповідно Закону України про авторське право і суміжні права N 3792-XII від 23 грудня 1993 року