Three-impulse point return orbit design for the manned lunar high-latitude exploration mission
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DOI: 10.1016/j.actaastro.2020.10.048
Abstract: Abstract A three-impulse point return orbit design method is proposed for the manned lunar high-latitude exploration mission. First, considering the restrictions of the reentry corridor and the landing point simultaneously, the constraint conditions of the… read more here.
Keywords: point return; three impulse; return orbit; orbit ... See more keywords