TY - GEN
T1 - Fault Tolerant Control for Engine Fuel System with Performance Degradation
AU - Zhang, Xinyuan
AU - Zhang, Yuwei
AU - Wang, Xingjian
AU - Wang, Shaoping
N1 - Publisher Copyright:
© 2025 IEEE.
PY - 2025
Y1 - 2025
N2 - In this paper, an adaptive fault-tolerant control (AFTC) strategy is designed for the fuel regulation system of aircraft engines with degraded performance, aiming to avoid saturation and instability problems that may be induced by the rash introduction of control instructions that exceed the system capabilities after the system performance is degraded. A multi-level fault quantification method is first proposed, mapping variations in key system parameters to five discrete fault severity levels. A hierarchical reference-model framework is then established: the open-loop system is linearized around each equilibrium point and closed with a simple segmented PID controller to form the reference models. Simulation studies comparing the step responses of both the reference model and the actual system under all five fault levels demonstrate that the proposed method maintains good stability and satisfactory tracking performance despite increasing fault severity. The results validate the feasibility and robustness of the multi-level reference model-based AFTC approach for fuel regulation systems, offering valuable insights for engineering implementation.
AB - In this paper, an adaptive fault-tolerant control (AFTC) strategy is designed for the fuel regulation system of aircraft engines with degraded performance, aiming to avoid saturation and instability problems that may be induced by the rash introduction of control instructions that exceed the system capabilities after the system performance is degraded. A multi-level fault quantification method is first proposed, mapping variations in key system parameters to five discrete fault severity levels. A hierarchical reference-model framework is then established: the open-loop system is linearized around each equilibrium point and closed with a simple segmented PID controller to form the reference models. Simulation studies comparing the step responses of both the reference model and the actual system under all five fault levels demonstrate that the proposed method maintains good stability and satisfactory tracking performance despite increasing fault severity. The results validate the feasibility and robustness of the multi-level reference model-based AFTC approach for fuel regulation systems, offering valuable insights for engineering implementation.
KW - aircraft fuel system
KW - fault-tolerant control
KW - performance degradation reference models
UR - https://www.scopus.com/pages/publications/105018096925
U2 - 10.1109/ICIEA65512.2025.11148841
DO - 10.1109/ICIEA65512.2025.11148841
M3 - 会议稿件
AN - SCOPUS:105018096925
T3 - 2025 IEEE 20th Conference on Industrial Electronics and Applications, ICIEA 2025
BT - 2025 IEEE 20th Conference on Industrial Electronics and Applications, ICIEA 2025
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 20th IEEE Conference on Industrial Electronics and Applications, ICIEA 2025
Y2 - 3 August 2025 through 6 August 2025
ER -