TY - GEN
T1 - Automatic Generation of Fault Diagnostic Reports for Satellite Parameters Based on Telemetry Data
AU - Pan, Meijia
AU - Wang, Ning
AU - Zhang, Ke
AU - Wang, Zhenhua
N1 - Publisher Copyright:
© The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd. 2025.
PY - 2025
Y1 - 2025
N2 - This paper investigates the fault diagnosis methodology of satellite star sensor and gyroscope utilizing telemetry data, alongside the exploration of automated fault diagnosis report generation through MATLAB. Initially, the consistency of measurements from multiple star sensors is evaluated using a star sensor data consistency algorithm, facilitating the detection of potential sensor failures. Upon confirming the normal operation of the star sensors, a star sensor-gyroscope combined diagnostic algorithm is employed. This algorithm integrates satellite attitude kinematics equations with the Extended Kalman Filter (EKF) to assess the consistency between star sensor and gyroscope data, thereby determining the presence of gyroscope failures. Additionally, the 3σ rule is applied to set threshold values for residual evaluation. The effectiveness of the proposed methods is validated through numerical simulation. Moreover, this study delves into the technology for auto-generating research reports on the MATLAB platform. It can automatically read telemetry data and invoke the fault diagnosis algorithm to complete fault analysis efficiently, ultimately producing a detailed fault diagnosis report.
AB - This paper investigates the fault diagnosis methodology of satellite star sensor and gyroscope utilizing telemetry data, alongside the exploration of automated fault diagnosis report generation through MATLAB. Initially, the consistency of measurements from multiple star sensors is evaluated using a star sensor data consistency algorithm, facilitating the detection of potential sensor failures. Upon confirming the normal operation of the star sensors, a star sensor-gyroscope combined diagnostic algorithm is employed. This algorithm integrates satellite attitude kinematics equations with the Extended Kalman Filter (EKF) to assess the consistency between star sensor and gyroscope data, thereby determining the presence of gyroscope failures. Additionally, the 3σ rule is applied to set threshold values for residual evaluation. The effectiveness of the proposed methods is validated through numerical simulation. Moreover, this study delves into the technology for auto-generating research reports on the MATLAB platform. It can automatically read telemetry data and invoke the fault diagnosis algorithm to complete fault analysis efficiently, ultimately producing a detailed fault diagnosis report.
KW - 3σ rule
KW - EKF
KW - auto-generating reports
KW - star sensor-gyroscope combined diagnostic algorithm
UR - https://www.scopus.com/pages/publications/105000819946
U2 - 10.1007/978-981-96-2212-2_35
DO - 10.1007/978-981-96-2212-2_35
M3 - 会议稿件
AN - SCOPUS:105000819946
SN - 9789819622115
T3 - Lecture Notes in Electrical Engineering
SP - 346
EP - 356
BT - Advances in Guidance, Navigation and Control - Proceedings of 2024 International Conference on Guidance, Navigation and Control Volume 4
A2 - Yan, Liang
A2 - Duan, Haibin
A2 - Deng, Yimin
PB - Springer Science and Business Media Deutschland GmbH
T2 - International Conference on Guidance, Navigation and Control, ICGNC 2024
Y2 - 9 August 2024 through 11 August 2024
ER -