Ensuring Survivability of Spacecraft Attitude Control System at Failures in Flywheel Cluster
A method for ensuring the survivability of a spacecraft attitude control system with minimally redundant cluster of the flywheels and magnetic actuator at the faults of any reaction wheels are presented. The results of computer simulation were obtained and it was found if any two of the four fly...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Hezarfen Aeronautics and Space Technologies Institue
2021-01-01
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| Series: | Havacılık ve Uzay Teknolojileri Dergisi |
| Subjects: | |
| Online Access: | http://jast.hho.edu.tr/index.php/JAST/article/view/434 |
| Summary: | A method for ensuring the survivability of a spacecraft attitude control
system with minimally redundant cluster of the flywheels and
magnetic actuator at the faults of any reaction wheels are presented.
The results of computer simulation were obtained and it was found if
any two of the four flywheels according to the General Electric
scheme fail, digital control of the flywheel cluster and magnetic drive
allows the land-survey satellite to maintain the ability for observation
of given terrestrial targets. |
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| ISSN: | 1304-0448 |