Fault Diagnosis and Reconfigurable Control for Commercial Aircraft with Multiple Faults and Actuator Saturation - Archive ouverte HAL Accéder directement au contenu
Article Dans Une Revue Aerospace Année : 2021

Fault Diagnosis and Reconfigurable Control for Commercial Aircraft with Multiple Faults and Actuator Saturation

(1) , (1) , (2, 3, 4) , (1)
1
2
3
4
Yishi Liu
Sheng Hong
Jianwei Liu
  • Fonction : Auteur

Résumé

Active fault-tolerant control systems perform fault diagnosis and reconfigurable control. There is a bidirectional uncertainty between them, and an integrated scheme is proposed here to account for that. The system considers both actuator and sensor faults, as well as the external disturbance. The diagnostic module is designed using an unknown input observer, and the controller is constructed on the basis of an adaptive method. The integrated strategy is presented, and the stability of the overall system is analyzed. Moreover, different kinds of anti-windup techniques are utilized to modify the original controllers, because of the different controller structures. A simulation of the integrated anti-windup fault-tolerant control method is demonstrated using a numerical model of Boeing 747. The results show that it can guarantee the stability of the post-fault aircraft and increase the control performance for the overall faulty system.

Dates et versions

hal-03474882 , version 1 (10-12-2021)

Licence

Paternité - CC BY 4.0

Identifiants

Citer

Yishi Liu, Sheng Hong, Enrico Zio, Jianwei Liu. Fault Diagnosis and Reconfigurable Control for Commercial Aircraft with Multiple Faults and Actuator Saturation. Aerospace, 2021, 8 (4), pp.108. ⟨10.3390/aerospace8040108⟩. ⟨hal-03474882⟩
20 Consultations
0 Téléchargements

Altmetric

Partager

Gmail Facebook Twitter LinkedIn More