Design of generalized fault diagnosis observer and active adaptive fault tolerant controller for aircraft control system

This study aims to design a generalized fault diagnosis observer (GFDO) and an active fault tolerant control system (AFTCS) for external disturbances based on an aircraft control system and actuator faults. Unlike the traditional approach that assumes external disturbances are norm bounded, the Gron...

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Bibliographic Details
Main Authors: Han, Y. (Author), Sun, R. (Author), Wang, Y. (Author)
Format: Article
Language:English
Published: American Institute of Mathematical Sciences 2022
Subjects:
Online Access:View Fulltext in Publisher
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008 220425s2022 CNT 000 0 und d
020 |a 15471063 (ISSN) 
245 1 0 |a Design of generalized fault diagnosis observer and active adaptive fault tolerant controller for aircraft control system 
260 0 |b American Institute of Mathematical Sciences  |c 2022 
856 |z View Fulltext in Publisher  |u https://doi.org/10.3934/mbe.2022262 
520 3 |a This study aims to design a generalized fault diagnosis observer (GFDO) and an active fault tolerant control system (AFTCS) for external disturbances based on an aircraft control system and actuator faults. Unlike the traditional approach that assumes external disturbances are norm bounded, the Gronwall Lemma based on the external disturbances constraint condition is modelled to satisfy the system stability. Then, the GFDO is designed by two performance indices defined to simultaneously estimate system states and faults. In addition, the AFTCS is designed to obtain the desired performances in the fault case. When the fault is diagnosed by GFDO, the regular controller switches to AFTCS. Finally, an analysis of the performance of the proposed algorithm is discussed based on simulations of the F-18 aircraft control system, which illustrates the effectiveness and applicability of this method. © 2022 the Author(s). 
650 0 4 |a Active fault tolerant control 
650 0 4 |a actuator fault 
650 0 4 |a Actuator fault 
650 0 4 |a Actuators 
650 0 4 |a Adaptive control systems 
650 0 4 |a Aircraft control 
650 0 4 |a aircraft control system 
650 0 4 |a Aircraft control systems 
650 0 4 |a Controllers 
650 0 4 |a External disturbances 
650 0 4 |a Failure analysis 
650 0 4 |a Fault detection 
650 0 4 |a Fault diagnosis observers 
650 0 4 |a fault estimation 
650 0 4 |a Fault estimation 
650 0 4 |a Fault tolerance 
650 0 4 |a fault tolerant control 
650 0 4 |a Fault tolerant control systems 
650 0 4 |a Faults tolerant controls 
650 0 4 |a Flight control systems 
650 0 4 |a Performance 
650 0 4 |a System faults 
650 0 4 |a System stability 
700 1 |a Han, Y.  |e author 
700 1 |a Sun, R.  |e author 
700 1 |a Wang, Y.  |e author 
773 |t Mathematical Biosciences and Engineering