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 Δ v costs and their scattering for each delay time. Families of orbits around the Earth–Moon L 1 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.


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    Titel :

    Recovery of quasi-halo orbit missions in case of contingent station-keeping maneuver delay


    Beteiligte:

    Erschienen in:

    Acta Astronautica ; 165 ; 382-387


    Erscheinungsdatum :

    2019-09-14


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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