A Design Method for Redundant Microthruster Layout With Allocation Error

The microthruster is generally chosen as the actuator of the drag-free satellite control system, and the layout directly affects the stability of the satellite control. Due to the extremely rigorous objectives of drag-free control, a design method for the redundant thruster layout is proposed in thi...

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Bibliographic Details
Main Authors: Mingwei Chen, Chu Zhang, Jianwu He, Chao Yang, Li Duan, Qi Kang
Format: Article
Language:English
Published: Wiley 2024-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2024/7627257
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