TY - JOUR
T1 - Active Fault-Tolerant Strategy for Flight Vehicles
T2 - Transfer Learning-Based Fault Diagnosis and Fixed-Time Fault-Tolerant Control
AU - Zhao, Jiaxin
AU - Lu, Pingli
AU - Du, Changkun
AU - Cao, Fangfei
N1 - Publisher Copyright:
© 1965-2011 IEEE.
PY - 2024/2/1
Y1 - 2024/2/1
N2 - In this article, we focus on the issue of active fault-tolerant strategy in the context of hypersonic vehicles. The proposed approach involves addressing the challenges of transfer learning-based fault diagnosis and implementing fixed-time fault-tolerant control. Based on a serial coupling of the 1-D residual convolution neural networks with attention mechanism (ResCNN-ATT) and the long short-term memory networks with attention mechanism (LSTM-ATT), a fault diagnosis deep residual convolution LSTM attention (ResCNN-LSTM-ATT) network is proposed. To deal with the insufficient data fault diagnosis problem, transfer learning technique is utilized based on the constructed ResCNN-LSTM-ATT network. Based on fault diagnosis information, a fixed-time nonsingular terminal sliding mode controller is designed to guarantee system tracking performance in the presence of actuator damage. Simulation results are performed to show the effectiveness of the proposed method based on the hypersonic vehicle model of NASA Langley Research Center.
AB - In this article, we focus on the issue of active fault-tolerant strategy in the context of hypersonic vehicles. The proposed approach involves addressing the challenges of transfer learning-based fault diagnosis and implementing fixed-time fault-tolerant control. Based on a serial coupling of the 1-D residual convolution neural networks with attention mechanism (ResCNN-ATT) and the long short-term memory networks with attention mechanism (LSTM-ATT), a fault diagnosis deep residual convolution LSTM attention (ResCNN-LSTM-ATT) network is proposed. To deal with the insufficient data fault diagnosis problem, transfer learning technique is utilized based on the constructed ResCNN-LSTM-ATT network. Based on fault diagnosis information, a fixed-time nonsingular terminal sliding mode controller is designed to guarantee system tracking performance in the presence of actuator damage. Simulation results are performed to show the effectiveness of the proposed method based on the hypersonic vehicle model of NASA Langley Research Center.
KW - Active fault-tolerant control
KW - fixed-time nonsingular terminal sliding mode (TSM)
KW - transfer learning-based fault diagnosis
UR - http://www.scopus.com/inward/record.url?scp=85178044703&partnerID=8YFLogxK
U2 - 10.1109/TAES.2023.3333763
DO - 10.1109/TAES.2023.3333763
M3 - Article
AN - SCOPUS:85178044703
SN - 0018-9251
VL - 60
SP - 1047
EP - 1059
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
IS - 1
ER -