Abstract The strategy developed by the authors in previous works for recovering halo orbit missions in case of contingent station-keeping maneuver delay is now applied to quasi-halo orbit missions. Monte Carlo trials are used to estimate recovery costs and their scattering for each delay time. Families of orbits around the Earth–Moon point are considered.
Highlights The problem of quasi-halo orbit mission recovery is considered. Optimal transfers to the reference and best backup quasi-halo orbits are compared. The adaptation scheme to the ephemeris model of motion is given. In the ephemeris model, the results change significantly and depend on the dates. Best target orbit in the CR3BP model can be not optimal in the ephemeris model.
Recovery of quasi-halo orbit missions in case of contingent station-keeping maneuver delay
Acta Astronautica ; 165 ; 382-387
2019-09-14
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Recovery of halo orbit missions in case of contingent station-keeping maneuver delay
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