TY - GEN
T1 - Data-Driven Equivalent Space Aero-Engine Sensor Robust Fault Diagnosis
AU - Song, Yixiao
AU - Gou, Linfeng
AU - Zhang, Meng
AU - Huang, Yingzhi
AU - Chen, Yingxue
N1 - Publisher Copyright:
© 2023 IEEE.
PY - 2023
Y1 - 2023
N2 - Aeroengine control system is the key to ensure the stable and efficient operation of the engine within the flight envelope. Due to long-Term work in harsh environments such as high temperature and high pressure, strong vibration, and electromagnetic interference, sensors are the most prone to failure components in the control system, which has a huge impact on control performance. In this paper, the sensor in the aero-engine control system is taken as the research object, and the fault diagnosis method based on data-driven is carried out. Aiming at the dynamic process of small deviation of aero-engine, first construct the method of solving the equivalent space of the system through engine data simplification and reduce the order, then design the equivalent vector through the robust performance index, and obtain the residual error generation for sensor fault detection Finally, the equivalent space is properly transformed, and the sensor fault reconstruction scheme is designed through the robust performance index. Simulation results show that the designed robust fault estimation and reconstruction scheme is effective for single sensor faults, and the fault diagnosis scheme has certain robustness.
AB - Aeroengine control system is the key to ensure the stable and efficient operation of the engine within the flight envelope. Due to long-Term work in harsh environments such as high temperature and high pressure, strong vibration, and electromagnetic interference, sensors are the most prone to failure components in the control system, which has a huge impact on control performance. In this paper, the sensor in the aero-engine control system is taken as the research object, and the fault diagnosis method based on data-driven is carried out. Aiming at the dynamic process of small deviation of aero-engine, first construct the method of solving the equivalent space of the system through engine data simplification and reduce the order, then design the equivalent vector through the robust performance index, and obtain the residual error generation for sensor fault detection Finally, the equivalent space is properly transformed, and the sensor fault reconstruction scheme is designed through the robust performance index. Simulation results show that the designed robust fault estimation and reconstruction scheme is effective for single sensor faults, and the fault diagnosis scheme has certain robustness.
KW - Aero-engine
KW - Data-driven
KW - Robust Fault Estimation
KW - Robust Fault Reconstruction
KW - Sensor fault diagnosis
UR - http://www.scopus.com/inward/record.url?scp=85186743487&partnerID=8YFLogxK
U2 - 10.1109/ICMAE59650.2023.10424570
DO - 10.1109/ICMAE59650.2023.10424570
M3 - 会议稿件
AN - SCOPUS:85186743487
T3 - 2023 14th International Conference on Mechanical and Aerospace Engineering, ICMAE 2023
SP - 237
EP - 242
BT - 2023 14th International Conference on Mechanical and Aerospace Engineering, ICMAE 2023
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 14th International Conference on Mechanical and Aerospace Engineering, ICMAE 2023
Y2 - 18 July 2023 through 21 July 2023
ER -