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Astronomical Observatory, Nanjing, People's Republic of China
A Computational Method of the Combined Perturbations for the Orbit of the Close Orbit Terrestrial Satellite
A Computational Method of the Perturbation Theory in the Air Drag of Artificial Earth Satellite
A criterion for the linear stability of equilibrium points in the perturbed restricted three-body problem and applications in robe problem
A method of initial orbit determination for long arc
A note on the numerical method for conserving the Runge-Lenz vector
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