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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Vydané v:	Data Driven Control and Learning Systems Conference (Online) s. 1935 - 1940
Hlavní autori:	Xu, Nuo, Xia, Xiwang, Li, Zhaoxiong, He, Xiongfeng, Guo, Ning, Wang, Pengcheng, Zhang, Yonghe
Médium:	Konferenčný príspevok..
Jazyk:	English
Vydavateľské údaje:	IEEE 17.05.2024
Predmet:	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
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