A novel model of space electromagnetic docking is established to solve the problem of traditional plume contamination and short service life in this paper. A new modelling technique regarding space electromagnetic docking for CubeSat is proposed. The mathematical model with four core-containing energized solenoids is derived and simplified to the magnetic dipole far-field model of single-turn coil. Simplifying the magnetic dipole far-field model will yield the model of space electromagnetic docking, and the numerical simulation results also verify the reliability and feasibility of simplification process.


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    Titel :

    Dynamics modeling and simulation of space electromagnetic docking for CubeSat


    Beteiligte:
    Shi, Keke (Autor:in) / Sun, Zhaowei (Autor:in) / Liu, Chuang (Autor:in) / Ye, Dong (Autor:in)


    Erscheinungsdatum :

    01.07.2017


    Format / Umfang :

    451947 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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