The Guidance, Navigation, and Control (GN&C) function on the International Space Station (ISS) determines navigation parameters (state vector, attitude, angular rate, pointing data, time), maintains Station attitude (non propulsively as a rule but propulsively when necessary), executes translation and reboost maneuvers, and supports microgravity experiments by limiting accelerations. The accuracies to which GN&C is to perform its functions are summarized, and then the expected performance of the current GN&C design is described, including pointing accuracy. Attitude bounds are illustrated as a function of calendar date given the current (Revision D) station assembly sequence and schedule.


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    Titel :

    Space station GN&C overview for payloads


    Beteiligte:
    Treder, Alfred J. (Autor:in) / Bragg, Mary J. (Herausgeber:in) / El-Genk, Mohamed S. (Herausgeber:in)

    Kongress:

    Space technology and applications international forum -1999 ; 1999 ; Albuquerque, New Mexico (USA)


    Erschienen in:

    Erscheinungsdatum :

    22.01.1999


    Format / Umfang :

    9 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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