Quantitative analysis of the atmospheric density models applicable for determination of artificial satellite deceleration

Author:

Zhaborovskyi V. P.

Publisher

Allerton Press

Subject

Space and Planetary Science,Astronomy and Astrophysics

Reference16 articles.

1. GOST 25645.11584, “Earth upper atmosphere,” in Density Model for Project Ballistic Computations of Artificial Earth Satellites, 24.08.84. (M., 1984)

2. B. R. Bowman, B. R. Bowman, W. K. Tobiska, F. Marcos, and C. Huang, “A new empirical thermospheric density model JB2008 using new solar and geomagnetic indices,” in 37th COSPAR Scientific Assembly, Held 13–20 July 2008, in Montreal, Canada (2008), p. 367.

3. S. L. Bruinsma, N. Sanchez-Ortiz, E. Olmedo, and N. Gujarro, “Evaluation of the DTM-2009 thermosphere model for benchmarking purposes,” J. Space Weather Space Clim 2, A04 (2012).

4. S. L. Bruinsma, G. Thuillier, and F. Barlier, “The DTM-2000 empirical thermosphere model with new data assimilation and constraints at lower boundary: accuracy and properties,” Journal of Atmospheric and Solar-Terrestrial Physics 65, 1053–1070 (2003).

5. J. O. Cappellari, C. E. Velez, and A. J. Fuchs, Mathematical Theory of the Goddard Trajectory Determination System, GSFC Document X-582-76-77, Greenbelt, 1976.

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