Abstract The Monitor-E spacecraft executed uncontrolled flight due to emergency situation, no telemetry information on parameters of the spacecraft’s attitude motion being available. So, the problem arose to determine the spacecraft’s rotational motion from the accessible indirect information—the electric current provided by solar batteries. In this paper the integrated statistical technique is described, that allows one to solve this problem. The values of current, obtained over the time interval some tens of minutes long, have been processed simultaneously by the least squares method using the integration of the equations of spacecraft’s rotational motion. As a result of processing, the initial conditions of motion were estimated, and the spacecraft’s moments of inertia were updated, as well as the angles, specifying solar batteries position in the spacecraft-fixed coordinate system. The results of processing of 12 data sets are presented, which allowed us to reconstruct the actual rotational motion of the spacecraft.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Determination of parameters of rotational motion of the Monitor-E spacecraft from the telemetry data on solar batteries’ current


    Beteiligte:
    Davydov, A. A. (Autor:in) / Sazonov, V. V. (Autor:in)

    Erschienen in:

    Cosmic Research ; 47 , 5 ; 399-408


    Erscheinungsdatum :

    2009-10-01


    Format / Umfang :

    10 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    SPACECRAFT SOLAR BATTERIES OUTPUT CURRENT DETERMINATION METHOD

    SPIRIN ALEKSANDR IVANOVICH / BELYAEV MIKHAIL YUREVICH / RULEV DMITRIJ NIKOLAEVICH | Europäisches Patentamt | 2017

    Freier Zugriff


    Spacecraft telemetry and command

    Charles, F. J. / Larson, F. L. | NTRS | 1967