CLC number:
On-line Access: 2024-08-27
Received: 2023-10-17
Revision Accepted: 2024-05-08
Crosschecked: 2023-10-19
Cited: 0
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Changyi XU, Wenya LI, Xuhui LIU, Yong LI, Chao ZHANG. Micro-Newton scale variable thrust control technique and its noise problem for drag-free satellite platforms: a review[J]. Journal of Zhejiang University Science A, 2023, 24(10): 841-858.
@article{title="Micro-Newton scale variable thrust control technique and its noise problem for drag-free satellite platforms: a review",
author="Changyi XU, Wenya LI, Xuhui LIU, Yong LI, Chao ZHANG",
journal="Journal of Zhejiang University Science A",
volume="24",
number="10",
pages="841-858",
year="2023",
publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.A2300104"
}
%0 Journal Article
%T Micro-Newton scale variable thrust control technique and its noise problem for drag-free satellite platforms: a review
%A Changyi XU
%A Wenya LI
%A Xuhui LIU
%A Yong LI
%A Chao ZHANG
%J Journal of Zhejiang University SCIENCE A
%V 24
%N 10
%P 841-858
%@ 1673-565X
%D 2023
%I Zhejiang University Press & Springer
%DOI 10.1631/jzus.A2300104
TY - JOUR
T1 - Micro-Newton scale variable thrust control technique and its noise problem for drag-free satellite platforms: a review
A1 - Changyi XU
A1 - Wenya LI
A1 - Xuhui LIU
A1 - Yong LI
A1 - Chao ZHANG
J0 - Journal of Zhejiang University Science A
VL - 24
IS - 10
SP - 841
EP - 858
%@ 1673-565X
Y1 - 2023
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/jzus.A2300104
Abstract: High-precision detection in fundamental space physics, such as space gravitational wave detection, high-precision earth gravity field measurement, and reference frame drag effect measurement, is the key to achieving important breakthroughs in the scientific study of fundamental space physics. Acquiring high-precision measurements requires high-performance satellite platforms to achieve “drag-free control” in a near “pure gravity” flight environment. The critical technology for drag-free control is variable thrust control at the micro-Newton scale. thrust noise is the most important technical indicator for achieving drag-free flight. However, there is no literature about the current status and future prospects of variable thrust control based on thrust noise. Therefore, the micro-Newton variable thrust control technology and the thrust noise of the drag-free satellite platform are reviewed in this work. Firstly, the research status of micro-Newton scale variable thrust control technology and its applications to drag-free satellite platforms are introduced. Then, the noise problem is analyzed in detail and its solution is theoretically investigated in three aspects: “cross-basin flow problem,” “control problem,” and “system instability and multiple-coupled problem.” Finally, a systematic overview is presented and the corresponding suggested directions of research are discussed. This work provides detailed understanding and support for realizing low-noise variable thrust control in the next generation of drag-free satellites.
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