Cubesat ADCS model for preliminary design procedures within a concurrent design approach

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. T...

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Bibliographic Details
Main Authors: Annenkova, A., Biktimirov, S., Latyshev, K., Mahfouz, A., Mukhachev, P., Pritykin, D.
Format: Conference Proceeding
Language:English
Online Access:Get full text
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Summary: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.
ISSN:0094-243X
1551-7616
DOI:10.1063/1.5133295