Design of Attitude Control Servomechanisms with Fluid Ring and CMG for Rigid Satellite
Satellites cover a wide range of space missions as remote sensing. Accomplishment of the mission depends on satellite’s stability maintenance and direction. The main task of the attitude control system is to provide stability to the satellite against external disturbances. Such perturbations are cau...
Main Authors: | Saleh Akbaritabar, Reza Esmaelzadeh, Reza Zardashti |
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Format: | Article |
Language: | English |
Published: |
Instituto de Aeronáutica e Espaço (IAE)
2018-11-01
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Series: | Journal of Aerospace Technology and Management |
Subjects: | |
Online Access: | https://www.jatm.com.br/jatm/article/view/950 |
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