The design of fault-tolerant flight control within actuator control authority

Xiang Yu; Yu Fu; Youmin Zhang

doi:10.1109/CGNCC.2016.7829071

The design of fault-tolerant flight control within actuator control authority

Xiang Yu
, Yu Fu
, Youmin Zhang^*

^*Corresponding author for this work

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

Abstract

When faults of some flight actuators have occurred, the aggressive use of fault-free actuators is often caused. This study focuses on a fault-tolerant flight control (FTFC) scheme, which is capable of tolerating aircraft actuator failures and respecting the control authority of healthy actuators. Adaptive sliding mode control (ASMC) technique is exploited in the FTFC design to ensure that the amplitudes and rates of the healthy actuators remain within the limited ranges. Simulation studies of nonlinear Boeing 747 longitudinal model are carried out to validate the effectiveness of the proposed scheme.

Original language	English
Title of host publication	CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	1851-1856
Number of pages	6
ISBN (Electronic)	9781467383189
DOIs	https://doi.org/10.1109/CGNCC.2016.7829071
State	Published - 20 Jan 2017
Externally published	Yes
Event	7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016 - Nanjing, Jiangsu, China Duration: 12 Aug 2016 → 14 Aug 2016

Publication series

Name	CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference

Conference

Conference	7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016
Country/Territory	China
City	Nanjing, Jiangsu
Period	12/08/16 → 14/08/16

Keywords

Actuator amplitude and rate limits
Adaptive sliding mode control
Fault-tolerant flight control

Access to Document

10.1109/CGNCC.2016.7829071

Cite this

Yu, X., Fu, Y., & Zhang, Y. (2017). The design of fault-tolerant flight control within actuator control authority. In CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference (pp. 1851-1856). Article 7829071 (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CGNCC.2016.7829071

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title = "The design of fault-tolerant flight control within actuator control authority",

abstract = "When faults of some flight actuators have occurred, the aggressive use of fault-free actuators is often caused. This study focuses on a fault-tolerant flight control (FTFC) scheme, which is capable of tolerating aircraft actuator failures and respecting the control authority of healthy actuators. Adaptive sliding mode control (ASMC) technique is exploited in the FTFC design to ensure that the amplitudes and rates of the healthy actuators remain within the limited ranges. Simulation studies of nonlinear Boeing 747 longitudinal model are carried out to validate the effectiveness of the proposed scheme.",

keywords = "Actuator amplitude and rate limits, Adaptive sliding mode control, Fault-tolerant flight control",

author = "Xiang Yu and Yu Fu and Youmin Zhang",

note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016 ; Conference date: 12-08-2016 Through 14-08-2016",

year = "2017",

month = jan,

day = "20",

doi = "10.1109/CGNCC.2016.7829071",

language = "英语",

series = "CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

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address = "美国",

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Yu, X, Fu, Y & Zhang, Y 2017, The design of fault-tolerant flight control within actuator control authority. in CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference., 7829071, CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference, Institute of Electrical and Electronics Engineers Inc., pp. 1851-1856, 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016, Nanjing, Jiangsu, China, 12/08/16. https://doi.org/10.1109/CGNCC.2016.7829071

The design of fault-tolerant flight control within actuator control authority. / Yu, Xiang; Fu, Yu; Zhang, Youmin.
CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference. Institute of Electrical and Electronics Engineers Inc., 2017. p. 1851-1856 7829071 (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference).

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

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AU - Fu, Yu

AU - Zhang, Youmin

PY - 2017/1/20

Y1 - 2017/1/20

N2 - When faults of some flight actuators have occurred, the aggressive use of fault-free actuators is often caused. This study focuses on a fault-tolerant flight control (FTFC) scheme, which is capable of tolerating aircraft actuator failures and respecting the control authority of healthy actuators. Adaptive sliding mode control (ASMC) technique is exploited in the FTFC design to ensure that the amplitudes and rates of the healthy actuators remain within the limited ranges. Simulation studies of nonlinear Boeing 747 longitudinal model are carried out to validate the effectiveness of the proposed scheme.

AB - When faults of some flight actuators have occurred, the aggressive use of fault-free actuators is often caused. This study focuses on a fault-tolerant flight control (FTFC) scheme, which is capable of tolerating aircraft actuator failures and respecting the control authority of healthy actuators. Adaptive sliding mode control (ASMC) technique is exploited in the FTFC design to ensure that the amplitudes and rates of the healthy actuators remain within the limited ranges. Simulation studies of nonlinear Boeing 747 longitudinal model are carried out to validate the effectiveness of the proposed scheme.

KW - Actuator amplitude and rate limits

KW - Adaptive sliding mode control

KW - Fault-tolerant flight control

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DO - 10.1109/CGNCC.2016.7829071

M3 - 会议稿件

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T3 - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference

SP - 1851

EP - 1856

BT - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016

Y2 - 12 August 2016 through 14 August 2016

ER -

Yu X, Fu Y, Zhang Y. The design of fault-tolerant flight control within actuator control authority. In CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference. Institute of Electrical and Electronics Engineers Inc. 2017. p. 1851-1856. 7829071. (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference). doi: 10.1109/CGNCC.2016.7829071

The design of fault-tolerant flight control within actuator control authority

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