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- W2015647582 abstract "Abstract This paper develops generalized analytic solutions of relative spacecraft dynamics in the presence of arbitrary perturbations and presents new perturbation-invariant relative orbits. The extension of existing results is achieved by using non-osculating orbital elements, i.e. removing the constraint that the instantaneous velocity vector be tangential to an instantaneous Keplerian ellipse. Generalized planetary equations are developed and averaged to yield a non-osculating description of the long-term effects of first-order small perturbations. The generalized planetary equations are linearized, and expressions for the relative dynamics are presented in terms of non-osculating classical orbital element differences. The developed methodology is utilized to find previously undetected J 2 -invariant relative orbits." @default.
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- W2015647582 title "Generalized solutions for relative spacecraft orbits under arbitrary perturbations" @default.
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- W2015647582 doi "https://doi.org/10.1016/j.actaastro.2006.07.013" @default.
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