A spacecraft nutation inhibition method for low-orbit geomagnetic energy storage in-orbit delivery includes: S1, enabling a delivery connection rod to be slidably connected to two mass blocks in a length direction, and adjusting the center of mass of a spacecraft system to pass through a main connecting shaft; S2, respectively measuring, calibrating and adjusting the center of mass and the principal axis of inertia of the delivery connection rod that is to deliver the space target or de-orbit debris; S3, carrying out energy storage delivery; S4, respectively adjusting the center of mass and the moment of inertia of the delivery connection rod after delivering the space target or de-orbit debris; S5, carrying out energy dissipation and unloading; and S6, enabling the spacecraft system to prepare to grab the next space target or de-orbit debris and proceeding to the next delivery work cycle.


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    Titel :

    SPACECRAFT NUTATION INHIBITION METHOD FOR LOW-ORBIT GEOMAGNETIC ENERGY STORAGE IN-ORBIT DELIVERY


    Beteiligte:
    LI WENHAO (Autor:in) / ZHANG HENG (Autor:in) / FENG GUANHUA (Autor:in) / ZHANG CHEN (Autor:in) / YANG LEI (Autor:in) / LV LINLI (Autor:in)

    Erscheinungsdatum :

    2022-09-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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