Fault Diagnosis Algorithm Based on Adjustable Nonlinear PI State Observer and Its Application in UAV Fault Diagnosis
Aiming at the problem of fault diagnosis in continuous time systems, a kind of fault diagnosis algorithm based on adaptive nonlinear proportional integral (PI) observer, which can realize the effective fault identification, is studied in this paper. Firstly, the stability and stability conditions of...
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Online Access: | https://www.mdpi.com/1999-4893/14/4/119 |
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doaj-9dde1c3c900c493286d5a20b31d57db52021-04-08T23:02:00ZengMDPI AGAlgorithms1999-48932021-04-011411911910.3390/a14040119Fault Diagnosis Algorithm Based on Adjustable Nonlinear PI State Observer and Its Application in UAV Fault DiagnosisQing Miao0Juhui Wei1Jiongqi Wang2Yuyun Chen3School of Mathematics and Big Data, Foshan University, Foshan 528225, ChinaCollege of Liberal Arts and Sciences, National University of Defense Technology, Changsha 410073, ChinaSchool of Mathematics and Big Data, Foshan University, Foshan 528225, ChinaSchool of Mathematics and Big Data, Foshan University, Foshan 528225, ChinaAiming at the problem of fault diagnosis in continuous time systems, a kind of fault diagnosis algorithm based on adaptive nonlinear proportional integral (PI) observer, which can realize the effective fault identification, is studied in this paper. Firstly, the stability and stability conditions of fault diagnosis method based on the PI observer are analyzed, and the upper bound of the fault estimation error is given. Secondly, the fault diagnosis algorithm based on adjustable nonlinear PI observer is designed and constructed, it is analyzed and we proved that the upper bound of fault estimation under this algorithm is better than that of the traditional method. Finally, the L-1011 unmanned aerial vehicle (UAV) is taken as the experimental object for numerical simulation, and the fault diagnosis method based on adaptive observer factor achieves faster response speed and more accurate fault identification results.https://www.mdpi.com/1999-4893/14/4/119fault diagnosisnonlinear observeradaptive algorithmUAVparameter estimation |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Qing Miao Juhui Wei Jiongqi Wang Yuyun Chen |
spellingShingle |
Qing Miao Juhui Wei Jiongqi Wang Yuyun Chen Fault Diagnosis Algorithm Based on Adjustable Nonlinear PI State Observer and Its Application in UAV Fault Diagnosis Algorithms fault diagnosis nonlinear observer adaptive algorithm UAV parameter estimation |
author_facet |
Qing Miao Juhui Wei Jiongqi Wang Yuyun Chen |
author_sort |
Qing Miao |
title |
Fault Diagnosis Algorithm Based on Adjustable Nonlinear PI State Observer and Its Application in UAV Fault Diagnosis |
title_short |
Fault Diagnosis Algorithm Based on Adjustable Nonlinear PI State Observer and Its Application in UAV Fault Diagnosis |
title_full |
Fault Diagnosis Algorithm Based on Adjustable Nonlinear PI State Observer and Its Application in UAV Fault Diagnosis |
title_fullStr |
Fault Diagnosis Algorithm Based on Adjustable Nonlinear PI State Observer and Its Application in UAV Fault Diagnosis |
title_full_unstemmed |
Fault Diagnosis Algorithm Based on Adjustable Nonlinear PI State Observer and Its Application in UAV Fault Diagnosis |
title_sort |
fault diagnosis algorithm based on adjustable nonlinear pi state observer and its application in uav fault diagnosis |
publisher |
MDPI AG |
series |
Algorithms |
issn |
1999-4893 |
publishDate |
2021-04-01 |
description |
Aiming at the problem of fault diagnosis in continuous time systems, a kind of fault diagnosis algorithm based on adaptive nonlinear proportional integral (PI) observer, which can realize the effective fault identification, is studied in this paper. Firstly, the stability and stability conditions of fault diagnosis method based on the PI observer are analyzed, and the upper bound of the fault estimation error is given. Secondly, the fault diagnosis algorithm based on adjustable nonlinear PI observer is designed and constructed, it is analyzed and we proved that the upper bound of fault estimation under this algorithm is better than that of the traditional method. Finally, the L-1011 unmanned aerial vehicle (UAV) is taken as the experimental object for numerical simulation, and the fault diagnosis method based on adaptive observer factor achieves faster response speed and more accurate fault identification results. |
topic |
fault diagnosis nonlinear observer adaptive algorithm UAV parameter estimation |
url |
https://www.mdpi.com/1999-4893/14/4/119 |
work_keys_str_mv |
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1721533479714291712 |