In this thesis the attitude determination and control system (ADCS) of a small cubesat is developed in the context of the AlbaSat UniPD project. The ADCS is umulated using Matlab Simulink to verify the compliance with the selected mission and with the other subsystems.
Development of the ADCS of a 2U cubesat
BONATO, VITTORIO
2022/2023
Abstract
In this thesis the attitude determination and control system (ADCS) of a small cubesat is developed in the context of the AlbaSat UniPD project. The ADCS is umulated using Matlab Simulink to verify the compliance with the selected mission and with the other subsystems.File in questo prodotto:
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Bonato_Vittorio.pdf
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Utilizza questo identificativo per citare o creare un link a questo documento:
https://hdl.handle.net/20.500.12608/55230