Abstract
The aim of this paper is the development of a model to propagate space debris in the geostationary ring considering the \(J_2\) effect due to the Earth oblateness, the Sun and Moon perturbations, and the solar radiation pressure. We justify the importance of considering the \(J_2\) effect when propagating space debris independently of the ratio A / m for short and long-term propagation. We study the role of the Sun and the Moon in the period and amplitude of the inclination for different values of A / m. Thanks to the Hamiltonian formulation of the problem and the use of Poincaré’s variables it is possible to express the evolution of the space debris through a simplified dynamical system. We test and validate our obtained analytical solutions with the numerical ones, computed with a powerful integrator named NIMASTEP. We analyse the improvements obtained when we include the \(J_2\) effect and the third body perturbations by a rigorous comparison with a previous model, which only considers the solar radiation pressure. Finally, we study the effect of the area-to-mass ratio on short and long-term propagation.
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Acknowledgments
The work of D. Casanova was supported by the research project with reference CUD1315 in the organism Centro Universitario de la Defensa de Zaragoza, and by the Spanish Ministry of Economy and Competitiveness (Project No. ESP201344217-R). The work of A. Petit was supported by a FRIA Ph.D. grant in the Department of Mathematics at the University of Namur.
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Casanova, D., Petit, A. & Lemaître, A. Long-term evolution of space debris under the \(J_2\) effect, the solar radiation pressure and the solar and lunar perturbations. Celest Mech Dyn Astr 123, 223–238 (2015). https://doi.org/10.1007/s10569-015-9644-1
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DOI: https://doi.org/10.1007/s10569-015-9644-1