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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    Title :

    Development of 1U CubeSat attitude determination and control system simulator


    Contributors:

    Conference:

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


    Published in:

    Publication date :

    2021-09-13


    Size :

    11 pages





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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