Non-iterative angles-only initial relative orbit determination with J2 perturbations
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DOI: 10.1016/j.actaastro.2018.06.033
Abstract: Abstract An approximate solution to the angles-only initial relative orbit determination problem is developed and evaluated in the context of the two-body problem with J 2 perturbations. The algorithm is non-iterative and requires the singular… read more here.
Keywords: initial relative; relative orbit; angles initial; orbit determination ... See more keywords