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...

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Bibliographic Details
Main Authors: Saleh Akbaritabar, Reza Esmaelzadeh, Reza Zardashti
Format: Article
Language:English
Published: Instituto de Aeronáutica e Espaço (IAE) 2018-11-01
Series:Journal of Aerospace Technology and Management
Subjects:
Online Access:https://www.jatm.com.br/jatm/article/view/950