The paper considers the dynamics of a dual-spin nanosatellite with an internal rotor placed into movable module on elastic connections. The nanosatellite consists of two modules - a carrier body and a mobile module with a rapidly rotating internal rotor, which classifies the nanosatellite as a dual-spin spacecraft. The movable module is connected to the main module by flexible rods. Changing the length of these rods makes it possible to carry out angular displacements of the nanosatellite and, therefore, to control the attitude dynamics of the nanosatellite.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Attitude dynamics modeling of a dual-spin nanosatellite with an elastic longitudinal axis


    Contributors:


    Publication date :

    2022-05-23


    Size :

    3828130 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Attitude dynamics of a dual-spin nanosatellite with a gravitational damper

    Doroshin, Anton V. / Eremenko, Alexandr V. | Elsevier | 2023



    Attitude dynamics of the first Russian nanosatellite TNS-0

    Ovchinnikov, M.Yu | Online Contents | 2007


    Attitude dynamics of the first Russian nanosatellite TNS-0

    Ovchinnikov, M.Yu. / Ilyin, A.A. / Kupriynova, N.V. et al. | Elsevier | 2007


    Attitude dynamics of the first Russian nanosatellite TNS-0

    Ovchinnikov, M.Yu. / Ilyin, A.A. / Kupriynova, N.V. et al. | AIAA | 2006