Testing and validation of a Β; algorithm for cubesat satellites
For most satellite missions, it is essential to decrease the satellite angular velocity. The Β algorithm is a common algorithm to stabilize the spacecraft by using magnetorquers. Controlling the satellite using the magnetorquers is part of the attitude control subsystem detumbling mode. Due to...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Institute of Physics Publishing
2016
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| Online Access: | http://psasir.upm.edu.my/id/eprint/52941/1/article.pdf |