THE METHOD FOR FAST DETERMINATION OF GEOSTATIONARY ARTH SATELLITE ORBIT FROM ANGULAR COORDINATES MEASUREMENTS

Автор(и)

  • O. A. Bazyey Department of Astronomy, Odessa State University T.G.Shevchenko Park, Odessa 65014 Ukraine; Nikolayev Astronomical Observatory Observatorna 1, 54030 Mykolaiv, Ukraine, Україна
  • E. S. Sibiryakova Nikolayev Astronomical Observatory Observatorna 1, 54030 Mykolaiv, Ukraine, Україна
  • A. V. Shulga Nikolayev Astronomical Observatory Observatorna 1, 54030 Mykolaiv, Ukraine, Україна

DOI:

https://doi.org/10.18524/1810-4215.2005.18.98233

Ключові слова:

Satellites, optical observations, satellite orbits

Анотація

Classical Laplas method for determination of Keplerian orbital elements is described. The values obtained are improved by the method of differential corrections. The software has been provided and realizes such an algorithm to calculate orbital elements for high artificial Earth satellites. The approach suggested is used in processing artificial Earth satellites observations at Nikolayev Astronomical Observatory (NAO). Examples are given of orbit calculations for some geostationary satellites.

Посилання

Abalakin V.K., Aksenov E.P., Grebennikov E.A., Rjabov Y.A.: 1971, The reference manual on the celestial mechanics and astrodynamics, Nauka.

Aksenov E.P.: 1977, The theory of motion Earth artificial satellites, Nauka.

Escobal P.: 1965, Methods of orbit determination, New York-London-Sydney.

Kovalchuk A., Shulga A., Martynov M. in: Combined CCD observational method of GSS //"Extension and connection of reference frames using ground based technique", Nikolaev, 2001, p. 199-205.

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Опубліковано

2017-04-09

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