Arc-based and path-based formulations are proposed and compared for integrated spacecraft routing and trajectory optimization in servicing missions with en-route propellant replenishment.
A branch-and-cut-and-price approach for the pickup and delivery problem with shuttle routes
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Formulation and Analysis for Integrated Spacecraft Routing and Trajectory Design Problem
Arc-based and path-based formulations are proposed and compared for integrated spacecraft routing and trajectory optimization in servicing missions with en-route propellant replenishment.