Open AccessReorienting nanosatellites to a predefined attitude using angular displacements of movable modules
Author(s) -
Anton V. Doroshin,
A. V. Eryomenko
Publication year - 2021
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1745/1/012054
Subject(s) - precession , circular motion , orientation (vector space) , dynamics (music) , motion (physics) , attitude control , angular velocity , rotation around a fixed axis , physics , computer science , aerospace engineering , control theory (sociology) , control (management) , engineering , computer vision , classical mechanics , acoustics , artificial intelligence , astronomy , mathematics , geometry
The dynamics of the spatial motion of a nanosatellite with a movable module tilted relative to the main body is considered. Control laws are developed to implement attitude dynamics with suppressing the precession-nutational motion, as well to bringing the nanosatellite into a predefined spatial orientation.