A low-cost CubeSat ADCS simulator has been developed to support learning facilities of nanosatellite technology at the Department of Physics-Energy Engineering, Surya University. The simulator includes three degrees of freedom inertial platform and a CubeSat model contains affordable commercial electronic components. The simulator is completed with a Graphical User Interface (GUI) to help the user controlling the CubeSat conveniently. There are two control systems used in the simulator-open loop and closed loop using PID control. The open-loop control system succeeds to change CubeSat's attitude based on the user's command, but it still has ±32.6° angle deviation. Whereas the use of a closed-loop control system minimized the angle deviation to ±7.7°. The platform could demonstrate the attitude dynamic of 1U CubeSat, though these preliminary results could be improved with hardware optimization, e.g., the actuator and sensor.


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    Titel :

    Development of 1U CubeSat attitude determination and control system simulator


    Beteiligte:
    Suhandinata (Autor:in) / Setiawan, M. N. (Autor:in) / Kurniawan, Farohaji (Herausgeber:in) / Kurniawati, Frida (Herausgeber:in) / Bahri, Sayr (Herausgeber:in) / Santosa, Cahya Edi (Herausgeber:in) / Hasbi, Wahyudi (Herausgeber:in) / Septanto, Harry (Herausgeber:in) / Hermawan, Eddy (Herausgeber:in)

    Kongress:

    THE 8TH INTERNATIONAL SEMINAR ON AEROSPACE SCIENCE AND TECHNOLOGY – ISAST 2020 ; 2020 ; Bogor, Indonesia


    Erschienen in:

    Erscheinungsdatum :

    13.09.2021


    Format / Umfang :

    11 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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