The method of alternating integration and interpolation and its application to the determination and prediction of spacecraft orbits

Details The method of alternating integration and interpolation and its application to the determination and prediction of spacecraft orbits The method of alternating integration and interpolation and its application to the determination and prediction of spacecraft orbits

Jul 1983

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1983kosis..21..644i&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 21, July-Aug. 1983, p. 644-647. In Russian.

Physics

Interpolation, Numerical Integration, Orbit Calculation, Spacecraft Orbits, Orbital Elements, Scientific Satellites, Space Navigation, Zonal Harmonics

Scientific paper

Algorithms are developed for a numerical-analytical method, the method of alternating integration and interpolation, which is based on Taratynova's (1960) approach and can be used to calculate spacecraft orbital parameters in the ascending nodes. In this method, the orbital parameters are slowly varying functions of the loop number in the prediction interval as a whole, and only zonal harmonics are taken into account in the model of the earth's gravitational field. Attention is given to results regarding the application of this method to the problem of ballistic-navigation support for certain scientific satellites.

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