Optimal two-impulse rendezvous transfers between elliptic orbits form continuous families that can be traced and classified via numerical continuation on first-order optimality conditions.
Two-phase framework for near-optimal multi-target Lambert rendezvous
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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.
citing papers explorer
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Families of Two-Impulse Optimal Rendezvous Transfers Between Elliptic Orbits
Optimal two-impulse rendezvous transfers between elliptic orbits form continuous families that can be traced and classified via numerical continuation on first-order optimality conditions.
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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.