On-Orbit Identification of Unstable Micro-Propulsion System Parameters Using Drag-Free Control

Space gravitational wave detection spacecraft is equipped with a drag-free control and micro-propulsion system, and adopts thrust closed-loop feedback control structure. An on-orbit high accuracy estimation algorithm of micro-thruster parameters based on drag-free control model is proposed in this p...

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Veröffentlicht in:	Data Driven Control and Learning Systems Conference (Online) S. 1935 - 1940
Hauptverfasser:	Xu, Nuo, Xia, Xiwang, Li, Zhaoxiong, He, Xiongfeng, Guo, Ning, Wang, Pengcheng, Zhang, Yonghe
Format:	Tagungsbericht
Sprache:	Englisch
Veröffentlicht:	IEEE 17.05.2024
Schlagworte:	Accuracy Attitude control Drag-free Control Fading channels Gravitational Waves Heuristic algorithms Micro-propulsion Recursive Least Square Simulation Space vehicles Thrust Identification Torque
ISSN:	2767-9861
Online-Zugang:	Volltext
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