Determining parameters of Moon’s orbital and rotational motion from LLR observations using GRAIL and IERS-recommended models

Author:

Pavlov Dmitry A.,Williams James G.,Suvorkin Vladimir V.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Astronomy and Astrophysics,Applied Mathematics,Computational Mathematics,Mathematical Physics,Modeling and Simulation

Reference41 articles.

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2. Bizouard, C., Gambis, D.: The combined solution C04 for earth orientation parameters consistent with international terrestrial reference frame 2005. In: Drewes, H. (ed.) Geodetic Reference Frames, IAG Symposium Munich, Germany, 9–14 October 2006, pp. 265–270. Springer, Berlin (2009)

3. Bizouard, C., Gambis, D.: The combined solution C04 for earth orientation parameters consistent with international terrestrial reference frame 2008. IERS notice (2011). http://hpiers.obspm.fr/iers/eop/eopc04/C04.guide.pdf

4. Chapront-Touzé, M., Chapront, J.: ELP 2000–85—a semi-analytical lunar ephemeris adequate for historical times. A&A 190(1–2), 342–352 (1998)

5. Cunningham, L.E.: On the computation of the spherical harmonic terms needed during the numerical integration of the orbital motion of an artificial satellite. Celest. Mech. 2(2), 207–216 (1970)

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