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...
Saved in:
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/ https://www.emerald.com/insight/content/doi/10.1108/AEAT-01-2020-0017/full/html |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Parameter Tuning Of An Active Force Control For Cmg-Based Controlled Small Satellite
by: Linghan, Samanaseh
Published: (2019) -
An optimum magnetic control torque generation of a momentum bias satellite
by: Suhadis, Nurulasikin, et al.
Published: (2014) -
New satellite attitude control structure using the geomagnetic field
by: Mohd Suhadis, Nurulasikin, et al.
Published: (2006) -
An optimum magnetic control torque generation of
a momentum bias satellite
by: Mohd Suhadis, Nurulasikin, et al.
Published: (2014) -
An optimum magnetic control torque generation of
a momentum bias satellite
by: Mohd Suhadis, Nurulasikin, et al.
Published: (2014)