When the number of CMGs is represented by n (n is an integer of 4 or more), (n-3) gimbal angles out of n gimbal angles corresponding to the n CMGs are set as free parameters, and an algebraic equation representing a relationship among three gimbal angles out of the n gimbal angles, the free parameters, and an angular momentum of all the CMGs is used to solve the algebraic equation while changing the free parameters within set ranges, to thereby obtain solutions of the gimbal angles of the plurality of CMGs required for achieving a given angular momentum.


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    Titel :

    DEVICE FOR CONTROLLING ATTITUDE OF SPACECRAFT AND METHOD FOR CALCULATING CMG GIMBAL ANGLE


    Weitere Titelangaben:

    VORRICHTUNG ZUR LAGESTEUERUNG EINES RAUMFAHRZEUGES UND VERFAHREN ZUR BERECHNUNG DES CMG-KARDANWINKELS
    DISPOSITIF PERMETTANT DE CONTRÔLER L'ATTITUDE D'UN ENGIN SPATIAL ET PROCÉDÉ PERMETTANT DE CALCULER L'ANGLE DE CARDAN D'ACTIONNEUR GYROSCOPIQUE (CMG)


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

    Erscheinungsdatum :

    23.01.2019


    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 / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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