An active force controlled of small CMG-based satellite
Purpose: This paper aims to investigate the attitude control pointing improvement for a small satellite with control moment gyroscopes (CMGs) using the active force control (AFC) method. Design/methodology/approach: The AFC method is developed with its governing equations and integrated into the con...
| Main Authors: | Salleh, Mohd Badrul, Mohd Suhadis, Nurulasikin, Varatharajoo, Renuganth |
|---|---|
| Format: | Article |
| Published: |
Emerald
2021
|
| Online Access: | http://psasir.upm.edu.my/id/eprint/95782/ |
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