An attitude determination and control system (ADCS) model is presented, which is used for CubeSat preliminary design stages in accordance with the European Space Agency (ESA) concurrent design approach. The model is implemented in Matlab/Simulink and integrated into the Concurrent Design Platform. The model’s performance is exemplified by a mission preliminary design conducted in the Concurrent Engineering Lab at Skoltech.
Cubesat ADCS model for preliminary design procedures within a concurrent design approach
XLIII ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration ; 2019 ; Moscow, Russia
AIP Conference Proceedings ; 2171 , 1
2019-11-15
12 pages
Conference paper
Electronic Resource
English
An Architecture Analysis of ADCS for CubeSat: A Recipe for ADCS Design of ICUBE
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