An attitude control device for space station with system parameter uncertainties and on-orbit dynamic disturbances. A plurality of state sensors measure a plurality of states of the space station. An identification frequency selecting device selects an identification frequency. A moment of inertia identification operator calculation unit calculates a moment of inertia identification operator. A moment of inertia identification device calculates moment of inertia of the space station. A disturbance torque identification device calculates disturbance torque. A control torque calculation unit calculates a control signal. A plurality of thrusters generate a control torque based on the control signal.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Attitude control device for space station with system parameter uncertainties and on-orbit dynamic disturbances


    Beteiligte:
    ANDOH FUKASHI (Autor:in)

    Erscheinungsdatum :

    11.08.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Orbit keeping attitude control for space station

    Barrows, D. / Bedell, H. | NTRS | 1983


    Attitude Control of Multiple Rigid Bodies with Uncertainties and Disturbances

    Xia, Yuanqing / Zhang, Jinhui / Lu, Kunfeng et al. | Springer Verlag | 2018



    Attitude Tracking of Rigid Spacecraft with Uncertainties and Disturbances

    Xia, Yuanqing / Fu, Mengyin | Springer Verlag | 2013