Robust method for determining the orbits of geostationary satellites with a lack of data

Authors

  • B.I. Demchenko Fesenkov Astrophysical Institute, Almaty, Kazakhstan
  • A.A. Komarov Al-Farabi Kazakh National University, Kazakstan, Almaty
  • L.A. Ussoltseva Fesenkov Astrophysical Institute, Almaty, Kazakhstan

Keywords:

Keplerian elements, spherical coordinates, criterion function, differential corrections

Abstract

The algorithm determining the Keplerian orbit elements GSS is presented taking into account a priori information. For it is proposed to use a regular system of elements Ei (i = 1, ..., 6). It is support system, free from that famous mathematical uncertainty elements of Kepler, which is associated with their non-orthogonality. Elements of the proposed support system are calculated by iterative method of differential corrections. In this case it is possible to consider a priori limitations and increase the stability of the algorithm.

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Published

2016-09-12

Issue

Vol. 2016 No. 3 (2016): Recent Contributions to Physics

Section

Nonlinear Physics. Radiophysics

How to Cite

[1]
B. Demchenko, A. Komarov, and L. Ussoltseva, “Robust method for determining the orbits of geostationary satellites with a lack of data”, Rec.Contr.Phys., vol. 2016, no. 3, pp. 120–124, Sep. 2016, Accessed: Jul. 07, 2026. [Online]. Available: https://bph.kaznu.kz/index.php/zhuzhu/article/view/922

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