Including the closed-form J2^2 effect in DSST
- Juan F. San-Juan 1
- Rosario López 1
- Iván Pérez 1
- Paul J. Cefola 2
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1
Universidad de La Rioja
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2
State University of New York
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- Carolin Frueh (ed. lit.)
- Renato Zanetti (ed. lit.)
- Jeffrey R. Stuart (ed. lit.)
- Angela L. Bowes (ed. lit.)
Editorial: Univelt Inc.
ISSN: 0065-3438, 1081-6003
ISBN: 978-0-87703-680-7, 978-0-87703-679-1
Año de publicación: 2021
Volumen: 176
Páginas: 3061 - 3076
Congreso: 31th AAS/AIAA Space Flight Mechanics Meeting held February (31º. 2021)
Tipo: Aportación congreso
beta Ver similares en nube de resultadosResumen
A second-order closed-form semi-analytical solution of the main problem of theartificial satellite theory (J2 contribution) consistent with the Draper SemianalyticSatellite Theory (DSST) is presented in Delaunay variables. The shortperiodterms are removed using an extension of the Lie-Deprit method. The averagedequations of motion are given explicitly and transformed into the nonsingularequinoctial elements. Finally, the second-order terms in the equations ofmotion are included in the C/C++ version of the DSST orbit propagator.