Synthesis of Control Algorithms of the Spacecraft Spatial Reorientation with the Use of Dynamic Equations of a Solid Body Rotational Motion in Rodrigo-Hamilton Parameters
Author:
Publisher
Begell House
Subject
Information Systems,Control and Systems Engineering,Software
Link
https://dl.begellhouse.com/download/article/73d4d4d646191957/01-16 - Yefimenko.pdf
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3. Modeling the disturbing effect on the aist small spacecraft based on the measurements data;Scientific Reports;2022-01-25
4. Modeling of centrifugal deployment of three-section minisatellite boom;Technical mechanics;2021-12-07
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