Guidance and control of satellite orientation when failures in flywheels cluster
Автор: Somov S.E., Somova T.E., Butyrin S.A., Somov E.I.
Журнал: Известия Самарского научного центра Российской академии наук @izvestiya-ssc
Рубрика: Информатика, вычислительная техника и управление
Статья в выпуске: 2 т.26, 2024 года.
Бесплатный доступ
The dynamic processes in attitude control of the Earth survey satellite when failures in the redundant cluster of flywheels and its reconfiguration are considered. The developed guidance and digital control algorithms are briefly presented, as well as the results of computer simulation demonstrating their effectiveness.
Spacecraft, guidance and attitude control, flywheel cluster, flywheel failure
Короткий адрес: https://sciup.org/148328691
IDR: 148328691 | DOI: 10.37313/1990-5378-2024-26-2-121-130
