When calculating a gimbal angle trajectory that satisfies boundary conditions set by an attitude boundary condition setter 2131 of the ground station 21, a gimbal angle trajectory calculator 2132 calculates the gimbal angle trajectory that minimizes a period of an acceleration interval within a range that satisfies driving restrictions of a gimbal, based on a gimbal angleof a start time and a gimbal angleof a fixed interval of an attitude change. Also, the gimbal angle trajectory is calculated that minimizes a period of a deceleration interval within a range that satisfies the driving restrictions of the gimbal, based on the gimbal angleof the fixed interval and a gimbal angleof a completion time of the attitude change. The obtained,,and an attitude change periodare transmitted to the artificial satellite as gimbal angle trajectory parameters, and the control moment gyros are controlled based on the gimbal angle trajectory parameters.


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    Titel :

    POSTURE CONTROL DEVICE, POSTURE CONTROL SYSTEM, GROUND STATION, ARTIFICIAL SATELLITE, METHOD FOR CONTROLLING POSTURE, AND PROGRAM


    Weitere Titelangaben:

    POSITIONSSTEUERUNGSVORRICHTUNG, POSITIONSSTEUERUNGSSYSTEM, BODENSTATION, KÜNSTLICHER SATELLIT, VERFAHREN ZUR STEUERUNG DER POSITION UND PROGRAMM
    DISPOSITIF DE COMMANDE DE POSTURE, SYSTÈME DE COMMANDE DE POSTURE, STATION AU SOL, SATELLITE ARTIFICIEL, PROCÉDÉ DE COMMANDE DE POSTURE, ET PROGRAMME


    Beteiligte:
    KITAMURA KENJI (Autor:in) / SHIMA TAKEYA (Autor:in) / YAMADA KATSUHIKO (Autor:in)

    Erscheinungsdatum :

    11.09.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS



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