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Publishing Language: Chinese | Open Access

On-orbit fault diagnosis and location method for the propulsion system of the TianTuo -5 satellite

Yong ZHAO1Zongyu WU1( )Haopeng LIANG1Tao SHENG1Zhishuai SHEN2Xuan ZHOU3
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China
Shanghai Institute of Space Propulsion, Shanghai 201100, China
Shandong Institute of Space Electronic Technology, Yantai 264000, China
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Abstract

In order to ensure the successful on-orbit scientific test mission of TianTou -5 satellite, the possible risks of each component of the satellite propulsion system were systematically and comprehensively evaluated from the perspectives of incidence and severity by using failure mode and impact analysis methods. According to the working characteristics of the satellite propulsion system, a set of fault detection and location methods were proposed according to its on-orbit working state and standby state respectively. The effectiveness of the method is verified in the on-orbit practice, and the healthy operation of TianTuo -5 is successfully guaranteed, and valuable experience is accumulated for the fault diagnosis of the satellite propulsion system in the future.

CLC number: V43 Document code: A Article ID: 1001-2486(2024)05-141-09

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Journal of National University of Defense Technology
Pages 141-149

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Cite this article:
ZHAO Y, WU Z, LIANG H, et al. On-orbit fault diagnosis and location method for the propulsion system of the TianTuo -5 satellite. Journal of National University of Defense Technology, 2024, 46(5): 141-149. https://doi.org/10.11887/j.cn.202405015

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Received: 25 October 2023
Published: 28 October 2024
© 2024 Journal of National University of Defense Technology

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).