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 :

    A plan for spacecraft automated rendezvous


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

    Erscheinungsdatum :

    01.10.1992


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Plan for Spacecraft Automated Rendezvous

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


    Automated Rendezvous and Docking of Spacecraft

    Kemble, Stephen | SAGE Publications | 2007




    Automated Rendezvous and Docking of Spacecraft

    Kemble, Stephen | Online Contents | 2007