| Autor: |
Suhandinata, Setiawan, M. N. |
| Předmět: |
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| Zdroj: |
AIP Conference Proceedings; 2021, Vol. 2366 Issue 1, p1-11, 11p |
| Abstrakt: |
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. [ABSTRACT FROM AUTHOR] |
| Databáze: |
Complementary Index |
| Externí odkaz: |
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