Attitude Maneuver and Stability Control of Hyper-Agile Satellite Using Reconfigurable Control Moment Gyros

Attitude Maneuver and Stability Control of Hyper-Agile Satellite Using Reconfigurable Control Moment Gyros

Addressing the problems of insurmountable unknown frictional disturbance and balancing the trade-off between high maneuverability and stability during attitude maneuver are important in low-cost miniaturized single control moment gyro clusters (SGCMGs) for hyper-agile satellite. This paper proposes...

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Bibliographic Details
Main Authors: Zhi Qu, Gaofei Zhang, Ziyang Meng, Kai Xu, Ruiqin Xu, Jiaojiao Di
Format: Article
Language:English
Published: MDPI AG 2022-06-01
Series:Aerospace
Subjects:
hyper-agile satellite
SGCMGs
reconfiguration design
octagonal cone-type
evaluation metrics
Online Access:https://www.mdpi.com/2226-4310/9/6/303

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https://www.mdpi.com/2226-4310/9/6/303

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