An automated rendezvous approach has been developed that utilizes advances in technology to reduce real-time/near real-time flight operations support personnel to an acceptable level that is near the minimum without jeopardizing the success of the mission. The on-board flight targeting uses a rule-based system to select the pursuit vehicle phasing orbits and uses precise navigation updates from the pursuit/target spacecraft made possible by the global positioning system receivers/processors on both spacecraft to adjust the phasing orbits and achieve rendezvous. The ascent-to-orbit targeting for the pursuit vehicle has been successfully decoupled from the on-orbit orbit transfer phasing targeting. Typical launch window data have been developed for the heavy lift launch vehicle and cargo transfer vehicle for a Space Station Freedom rendezvous mission.


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    Titel :

    Plan for Spacecraft Automated Rendezvous


    Beteiligte:
    A. W. Deaton (Autor:in) / J. J. Lomas (Autor:in) / L. D. Mullins (Autor:in)

    Erscheinungsdatum :

    1992


    Format / Umfang :

    64 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    A plan for spacecraft automated rendezvous

    Deaton, A. W. / Lomas, J. J. / Mullins, L. D. | NTRS | 1992



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