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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Dynamics modeling and simulation of space electromagnetic docking for CubeSat


    Contributors:
    Shi, Keke (author) / Sun, Zhaowei (author) / Liu, Chuang (author) / Ye, Dong (author)


    Publication date :

    2017-07-01


    Size :

    451947 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Non-rod-cone type modularized cubesat electromagnetic docking mechanism

    YAO ZUNHAO / LIU BOFEI / YE DONG | European Patent Office | 2024

    Free access



    Optical design of small space rendezvous and docking lens for CubeSat

    Lin, Sheng-feng / Hsieh, Ting-Heng / Tung, Jung-Chen | SPIE | 2020


    Optical design of small space rendezvous and docking lens for CubeSat

    Lin, Sheng-feng / Hsieh, Ting-Heng / Tung, Jung-Chen | British Library Conference Proceedings | 2020