Fault Detection and Diagnosis of Aircraft Electro Hydrostatic Actuator Control System

Yinchao Chen; Zhenling Mo; Lei Xie; Qiang Miao

doi:10.1109/PHM-Chongqing.2018.00172

Fault Detection and Diagnosis of Aircraft Electro Hydrostatic Actuator Control System

Yinchao Chen, Zhenling Mo, Lei Xie, Qiang Miao

Research output: Chapters, Conference Papers, Creative and Literary Works › RGC 32 - Refereed conference paper (with host publication) › peer-review

5 Citations (Scopus)

Abstract

Electro hydrostatic actuator (EHA) is a key component of the actuation control system of modern aircraft. In order to maintain a high level of safety, fault detection and diagnosis of EHA control system is of great importance even though some degree of redundancy in the system already exists. In this paper, some common and detectable faults/failures of EHA control system are summarized, and some useful model-based fault detection and diagnosis methods are reviewed and discussed in details. © 2018 IEEE.

Original language	English
Title of host publication	Proceedings - 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018
Publisher	IEEE
Pages	963-967
ISBN (Print)	9781538653791
DOIs	https://doi.org/10.1109/PHM-Chongqing.2018.00172
Publication status	Published - 4 Jan 2019
Externally published	Yes
Event	2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018 - Chongqing, China Duration: 26 Oct 2018 → 28 Oct 2018

Publication series

Name	Proceedings - 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018

Conference

Conference	2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018
Place	China
City	Chongqing
Period	26/10/18 → 28/10/18

Bibliographical note

Publication details (e.g. title, author(s), publication statuses and dates) are captured on an “AS IS” and “AS AVAILABLE” basis at the time of record harvesting from the data source. Suggestions for further amendments or supplementary information can be sent to [email protected].

Funding

This research was supported by National Defence Basic Scientific Research Projects under Grant No. JCKY 2016205A004.

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 7 Affordable and Clean Energy

Research Keywords

Aircraft
EHA
Failure mode
FDD
Observer

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10.1109/PHM-Chongqing.2018.00172

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Chen, Y., Mo, Z., Xie, L., & Miao, Q. (2019). Fault Detection and Diagnosis of Aircraft Electro Hydrostatic Actuator Control System. In Proceedings - 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018 (pp. 963-967). Article 8603480 (Proceedings - 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018). IEEE. https://doi.org/10.1109/PHM-Chongqing.2018.00172

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abstract = "Electro hydrostatic actuator (EHA) is a key component of the actuation control system of modern aircraft. In order to maintain a high level of safety, fault detection and diagnosis of EHA control system is of great importance even though some degree of redundancy in the system already exists. In this paper, some common and detectable faults/failures of EHA control system are summarized, and some useful model-based fault detection and diagnosis methods are reviewed and discussed in details. {\textcopyright} 2018 IEEE.",

keywords = "Aircraft, EHA, Failure mode, FDD, Observer",

author = "Yinchao Chen and Zhenling Mo and Lei Xie and Qiang Miao",

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Chen, Y, Mo, Z, Xie, L & Miao, Q 2019, Fault Detection and Diagnosis of Aircraft Electro Hydrostatic Actuator Control System. in Proceedings - 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018., 8603480, Proceedings - 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018, IEEE, pp. 963-967, 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018, Chongqing, China, 26/10/18. https://doi.org/10.1109/PHM-Chongqing.2018.00172

Fault Detection and Diagnosis of Aircraft Electro Hydrostatic Actuator Control System. / Chen, Yinchao; Mo, Zhenling; Xie, Lei et al.
Proceedings - 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018. IEEE, 2019. p. 963-967 8603480 (Proceedings - 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018).

Research output: Chapters, Conference Papers, Creative and Literary Works › RGC 32 - Refereed conference paper (with host publication) › peer-review

TY - GEN

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AU - Chen, Yinchao

AU - Mo, Zhenling

AU - Xie, Lei

AU - Miao, Qiang

N1 - Publication details (e.g. title, author(s), publication statuses and dates) are captured on an “AS IS” and “AS AVAILABLE” basis at the time of record harvesting from the data source. Suggestions for further amendments or supplementary information can be sent to [email protected].

PY - 2019/1/4

Y1 - 2019/1/4

N2 - Electro hydrostatic actuator (EHA) is a key component of the actuation control system of modern aircraft. In order to maintain a high level of safety, fault detection and diagnosis of EHA control system is of great importance even though some degree of redundancy in the system already exists. In this paper, some common and detectable faults/failures of EHA control system are summarized, and some useful model-based fault detection and diagnosis methods are reviewed and discussed in details. © 2018 IEEE.

AB - Electro hydrostatic actuator (EHA) is a key component of the actuation control system of modern aircraft. In order to maintain a high level of safety, fault detection and diagnosis of EHA control system is of great importance even though some degree of redundancy in the system already exists. In this paper, some common and detectable faults/failures of EHA control system are summarized, and some useful model-based fault detection and diagnosis methods are reviewed and discussed in details. © 2018 IEEE.

KW - Aircraft

KW - EHA

KW - Failure mode

KW - FDD

KW - Observer

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M3 - RGC 32 - Refereed conference paper (with host publication)

SN - 9781538653791

T3 - Proceedings - 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018

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BT - Proceedings - 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018

PB - IEEE

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ER -

Chen Y, Mo Z, Xie L, Miao Q. Fault Detection and Diagnosis of Aircraft Electro Hydrostatic Actuator Control System. In Proceedings - 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018. IEEE. 2019. p. 963-967. 8603480. (Proceedings - 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018). doi: 10.1109/PHM-Chongqing.2018.00172

Fault Detection and Diagnosis of Aircraft Electro Hydrostatic Actuator Control System

Abstract

Publication series

Conference

Bibliographical note

Funding

UN SDGs

Research Keywords

Access Output

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