The influence of application a simplified transformation model between reference frames ECEF and ECI onto prediction accuracy of position and velocity of GLONASS satellites

• Autorzy: Krzyżek R. , Skorupa B.

Identyfikatory

DOI

10.2478/rgg-2015-0009

• Języki publikacji: EN

Abstrakty

EN

In computational tasks of satellite geodesy there is a need for transformation of coordinates between reference frames ECEF – Earth Centered, Earth Fixed and ECI – Earth Centered, Inertial. Strict and simplified transformation models, which can be used in case of the position and velocity short-term predictions of GLONASS satellites, have been presented in this study. Comparison of the results of state vector components predictions of the GLONASS satellites, in dependence of the used transformation model, have also been presented. Accuracy of the prediction has been determined on the basis of the analyse of deviations of the predicted positions and velocities of GLONASS satellites from their values given in broadcast ephemeris.

Słowa kluczowe

EN

broadcast ephemeris; transformation; ECEF; ECI; GLONASS

PL

efemerydy; transmisja; transformacja; ECEF; ECI; GLONASS

• Wydawca: Wydział Geodezji i Kartografii Politechniki Warszawskiej
• Czasopismo: Reports on Geodesy and Geoinformatics
• Rocznik: 2015
• Tom: Vol. 99
• Strony: 19--27
• Opis fizyczny: Bibliogr. 8 poz., tab., wykr.

Twórcy

autor

Krzyżek R.

• AGH University of Science and Technology, Faculty of Mining Surveying and Environmental Engineering, Department of Geomatics, 30 Mickiewicza Av., 30-059 Krakow, Poland

autor

Skorupa B.

• AGH University of Science and Technology, Faculty of Mining Surveying and Environmental Engineering, Department of Geomatics, 30 Mickiewicza Av., 30-059 Krakow, Poland

Bibliografia

• [1] GLONASS Interface Control Document (5.1th ed.). (2008). Moscow. Retrieved
• [2] Góral, W., & Skorupa, B. (2012). Determination of intermediate orbit and position of GLONASS satellites based on the generalized problem of two fixed centers. Acta Geodynamica et Geomaterialia, 9(3), 283–290
• [3] Hsu, T. A., Wang, L. S., Chang, F. R., Tseng, Y. F. (2010). Long-term prediction of GPS satellite orbit. Proceedings of The Society of Instrument and Control Engineers Annual Conference, Taipei, Taiwan, 2906-2909
• [4] Kryński, J. (Eds.).(2004). Nowe obowiązujące niebieskie i ziemskie systemy i układy odniesienia oraz ich wzajemne relacje. Warszawa: Instytut Geodezji i Kartografii
• [5] Montenbruck, O., Gill, E. (2000). Satellite Orbits - Models, Methods and Applications. Heidelberg: Springer-Verlag
• [6] Seeber, G. (2003). Satellite Geodesy: Foundation, Methods & Applications. Berlin - New York: Walter de Gruyter
• [7] Vallado, A. D. (2007). Fundamentals of Astrodynamics and Applications. (3rd ed.) New York: Springer-Verlag
• [8] Xu, G. (2008). Orbits. Berlin: Springer-Verlag