Enhanced attitude control structure for small satellites with reaction wheels
Purpose: This paper aims to describe a design enhancement for the satellite attitude control system using reaction wheels, and the wheel momentum unloading using magnetorquers. Design/methodology/approach: The proportional – integral–derivative-controller and active force control (AFC) schemes are d...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Emerald
2015
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| Online Access: | http://psasir.upm.edu.my/id/eprint/44624/1/Enhanced%20attitude%20control%20structure%20for%20small%20satellites%20with%20reaction%20wheels.pdf http://psasir.upm.edu.my/id/eprint/44624/ https://www.emerald.com/insight/content/doi/10.1108/AEAT-06-2014-0085/full/html |
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