Nonlinear analytic solution for perturbed relative motion using differential equinoctial elements
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DOI: 10.1007/s10569-018-9855-3
Abstract: This paper develops a nonlinear analytic solution for satellite relative motion in J2-perturbed elliptic orbits by using the geometric method that can avoid directly solving the complex differential equations. The differential equinoctial elements (DEEs) are… read more here.
Keywords: nonlinear analytic; relative motion; analytic solution; differential equinoctial ... See more keywords