With the development of space technology, the missions of modern satellites are becoming more complicated. Therefore, it is essential to maintain a satellite’s attitude to perform specific missions successfully. Sending satellites into space is time-consuming and expensive, making their on-ground testing necessary and crucial. This paper proposes a hardware-in-the-loop simulation system to verify the satellite attitude control system. The hardware-in-the-loop simulation system is a low-cost solution for mimicking a gravity-free environment, allowing the satellite attitude control to perform as it will be in space.


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    Titel :

    Design of a Nanosatellite Attitude Control Hardware-in-the-loop Simulation System


    Beteiligte:
    Lee, Yong-Seok (Autor:in) / Xuan-Mung, Nguyen (Autor:in) / Do, Truong-Dong (Autor:in) / Park, Joon-Young (Autor:in) / Lee, Choong-Hyun (Autor:in) / Hong, Sung Kyung (Autor:in)


    Erscheinungsdatum :

    27.07.2023


    Format / Umfang :

    774547 byte





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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