Reliability assessment of aircraft power and actuation system based on three-axis control

Xiaoyu Cui; Shaoping Wang; Qian Li; Jian Shi

doi:10.1109/AIM.2015.7222562

Reliability assessment of aircraft power and actuation system based on three-axis control

Xiaoyu Cui^*
, Shaoping Wang
, Qian Li
, Jian Shi

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Beihang University

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

8 Scopus citations

Abstract

As a key subsystem in aircraft, electro-hydraulic power and actuation system embodies performance and reliability that is crucial to aircraft safety, maneuverability and flight quality. The substantially increased system redundancy and high volume of dissimilar redundancy further complicate the aircraft electro-hydraulic control and actuation system. This paper presents the reliability model based on three-axis control as well as the reliability assessment method considering the function and performance. Application in several structures of aircraft power and actuation system indicates that the results of proposed method are closer to the actual situation.

Original language	English
Title of host publication	AIM 2015 - 2015 IEEE/ASME International Conference on Advanced Intelligent Mechatronics
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	382-387
Number of pages	6
ISBN (Electronic)	9781467391078
DOIs	https://doi.org/10.1109/AIM.2015.7222562
State	Published - 25 Aug 2015
Event	IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM 2015 - Busan, Korea, Republic of Duration: 7 Jul 2015 → 11 Jul 2015

Publication series

Name	IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM
Volume	2015-August

Conference

Conference	IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM 2015
Country/Territory	Korea, Republic of
City	Busan
Period	7/07/15 → 11/07/15

Keywords

dissimilar redundancy
power and actuation system
reliability assessment
three-axis control

Access to Document

10.1109/AIM.2015.7222562

Cite this

Cui, X., Wang, S., Li, Q., & Shi, J. (2015). Reliability assessment of aircraft power and actuation system based on three-axis control. In AIM 2015 - 2015 IEEE/ASME International Conference on Advanced Intelligent Mechatronics (pp. 382-387). Article 7222562 (IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM; Vol. 2015-August). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/AIM.2015.7222562

Cui, Xiaoyu ; Wang, Shaoping ; Li, Qian et al. / Reliability assessment of aircraft power and actuation system based on three-axis control. AIM 2015 - 2015 IEEE/ASME International Conference on Advanced Intelligent Mechatronics. Institute of Electrical and Electronics Engineers Inc., 2015. pp. 382-387 (IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM).

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title = "Reliability assessment of aircraft power and actuation system based on three-axis control",

abstract = "As a key subsystem in aircraft, electro-hydraulic power and actuation system embodies performance and reliability that is crucial to aircraft safety, maneuverability and flight quality. The substantially increased system redundancy and high volume of dissimilar redundancy further complicate the aircraft electro-hydraulic control and actuation system. This paper presents the reliability model based on three-axis control as well as the reliability assessment method considering the function and performance. Application in several structures of aircraft power and actuation system indicates that the results of proposed method are closer to the actual situation.",

keywords = "dissimilar redundancy, power and actuation system, reliability assessment, three-axis control",

author = "Xiaoyu Cui and Shaoping Wang and Qian Li and Jian Shi",

note = "Publisher Copyright: {\textcopyright} 2015 IEEE.; IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM 2015 ; Conference date: 07-07-2015 Through 11-07-2015",

year = "2015",

month = aug,

day = "25",

doi = "10.1109/AIM.2015.7222562",

language = "英语",

series = "IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM",

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Cui, X, Wang, S, Li, Q & Shi, J 2015, Reliability assessment of aircraft power and actuation system based on three-axis control. in AIM 2015 - 2015 IEEE/ASME International Conference on Advanced Intelligent Mechatronics., 7222562, IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM, vol. 2015-August, Institute of Electrical and Electronics Engineers Inc., pp. 382-387, IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM 2015, Busan, Korea, Republic of, 7/07/15. https://doi.org/10.1109/AIM.2015.7222562

Reliability assessment of aircraft power and actuation system based on three-axis control. / Cui, Xiaoyu; Wang, Shaoping; Li, Qian et al.
AIM 2015 - 2015 IEEE/ASME International Conference on Advanced Intelligent Mechatronics. Institute of Electrical and Electronics Engineers Inc., 2015. p. 382-387 7222562 (IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM; Vol. 2015-August).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Reliability assessment of aircraft power and actuation system based on three-axis control

AU - Cui, Xiaoyu

AU - Wang, Shaoping

AU - Li, Qian

AU - Shi, Jian

PY - 2015/8/25

Y1 - 2015/8/25

N2 - As a key subsystem in aircraft, electro-hydraulic power and actuation system embodies performance and reliability that is crucial to aircraft safety, maneuverability and flight quality. The substantially increased system redundancy and high volume of dissimilar redundancy further complicate the aircraft electro-hydraulic control and actuation system. This paper presents the reliability model based on three-axis control as well as the reliability assessment method considering the function and performance. Application in several structures of aircraft power and actuation system indicates that the results of proposed method are closer to the actual situation.

AB - As a key subsystem in aircraft, electro-hydraulic power and actuation system embodies performance and reliability that is crucial to aircraft safety, maneuverability and flight quality. The substantially increased system redundancy and high volume of dissimilar redundancy further complicate the aircraft electro-hydraulic control and actuation system. This paper presents the reliability model based on three-axis control as well as the reliability assessment method considering the function and performance. Application in several structures of aircraft power and actuation system indicates that the results of proposed method are closer to the actual situation.

KW - dissimilar redundancy

KW - power and actuation system

KW - reliability assessment

KW - three-axis control

UR - https://www.scopus.com/pages/publications/84951020722

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DO - 10.1109/AIM.2015.7222562

M3 - 会议稿件

AN - SCOPUS:84951020722

T3 - IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM

SP - 382

EP - 387

BT - AIM 2015 - 2015 IEEE/ASME International Conference on Advanced Intelligent Mechatronics

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM 2015

Y2 - 7 July 2015 through 11 July 2015

ER -

Cui X, Wang S, Li Q, Shi J. Reliability assessment of aircraft power and actuation system based on three-axis control. In AIM 2015 - 2015 IEEE/ASME International Conference on Advanced Intelligent Mechatronics. Institute of Electrical and Electronics Engineers Inc. 2015. p. 382-387. 7222562. (IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM). doi: 10.1109/AIM.2015.7222562

Reliability assessment of aircraft power and actuation system based on three-axis control

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