Ensuring the survivability of spacecraft control system at critical failures of reaction wheels
Автор: Somov S.Ye., Somova T.Ye.
Журнал: Известия Самарского научного центра Российской академии наук @izvestiya-ssc
Рубрика: Информатика, вычислительная техника и управление
Статья в выпуске: 2 т.23, 2021 года.
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A method for ensuring the survivability of the spacecraft attitude control system with a minimally redundant cluster of flywheels by General Electric scheme and a magnetic drive in the event of the flywheels’ failures is presented. The results of computer simulation were obtained and it was found that in case of failure of any two flywheels, the Earth survey satellite retains the ability to scanning observation given targets.
Spacecraft, attitude control, reaction wheels, failures, survivability
Короткий адрес: https://sciup.org/148322365
IDR: 148322365 | DOI: 10.37313/1990-5378-2021-23-2-66-74
