Active fault-Tolerant control strategy for lateral motion of civil aircraft

Kangle Wang; Shaoping Wang; Xingjian Wang; Zhongwei Yang

doi:10.1109/AUS.2016.7748145

Active fault-Tolerant control strategy for lateral motion of civil aircraft

Kangle Wang^*
, Shaoping Wang
, Xingjian Wang
, Zhongwei Yang

^*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

3 Scopus citations

Abstract

As civil aircrafts require high requirement of reliability, the flight control system should make airplane safe at least when failure occurs. This paper proposed an active fault-Tolerant control (AFTC) strategy for civil aircraft with ailerons stuck at different degrees. The baseline control law was designed based on linear quadratic regulator (LQR) to guarantee lateral control stability and performance. On this basis, a reconfigurable controller was designed based on model reference for the supposed failures. The simulation of lateral motion under the numerical model of Boeing 747 was carried out with the consideration of the impact of spoilers. Comparing the simulation results under reconfigurable controller with AFTC strategy and only under basic controller, the AFTC strategy was proved to be effective precisely.

Original language	English
Title of host publication	AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	713-718
Number of pages	6
ISBN (Electronic)	9781509010875
DOIs	https://doi.org/10.1109/AUS.2016.7748145
State	Published - 17 Nov 2016
Event	2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016 - Beijing, China Duration: 10 Oct 2016 → 12 Oct 2016

Publication series

Name	AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems

Conference

Conference	2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016
Country/Territory	China
City	Beijing
Period	10/10/16 → 12/10/16

Access to Document

10.1109/AUS.2016.7748145

Cite this

Wang, K., Wang, S., Wang, X., & Yang, Z. (2016). Active fault-Tolerant control strategy for lateral motion of civil aircraft. In AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems (pp. 713-718). Article 7748145 (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/AUS.2016.7748145

Wang, Kangle ; Wang, Shaoping ; Wang, Xingjian et al. / Active fault-Tolerant control strategy for lateral motion of civil aircraft. AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems. Institute of Electrical and Electronics Engineers Inc., 2016. pp. 713-718 (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems).

@inproceedings{f3cbfac7fa58498c93c1b68557477f70,

title = "Active fault-Tolerant control strategy for lateral motion of civil aircraft",

abstract = "As civil aircrafts require high requirement of reliability, the flight control system should make airplane safe at least when failure occurs. This paper proposed an active fault-Tolerant control (AFTC) strategy for civil aircraft with ailerons stuck at different degrees. The baseline control law was designed based on linear quadratic regulator (LQR) to guarantee lateral control stability and performance. On this basis, a reconfigurable controller was designed based on model reference for the supposed failures. The simulation of lateral motion under the numerical model of Boeing 747 was carried out with the consideration of the impact of spoilers. Comparing the simulation results under reconfigurable controller with AFTC strategy and only under basic controller, the AFTC strategy was proved to be effective precisely.",

author = "Kangle Wang and Shaoping Wang and Xingjian Wang and Zhongwei Yang",

note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016 ; Conference date: 10-10-2016 Through 12-10-2016",

year = "2016",

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language = "英语",

series = "AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems",

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address = "美国",

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Wang, K, Wang, S , Wang, X & Yang, Z 2016, Active fault-Tolerant control strategy for lateral motion of civil aircraft. in AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems., 7748145, AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, Institute of Electrical and Electronics Engineers Inc., pp. 713-718, 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016, Beijing, China, 10/10/16. https://doi.org/10.1109/AUS.2016.7748145

Active fault-Tolerant control strategy for lateral motion of civil aircraft. / Wang, Kangle; Wang, Shaoping ; Wang, Xingjian et al.
AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems. Institute of Electrical and Electronics Engineers Inc., 2016. p. 713-718 7748145 (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems).

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

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AU - Yang, Zhongwei

PY - 2016/11/17

Y1 - 2016/11/17

N2 - As civil aircrafts require high requirement of reliability, the flight control system should make airplane safe at least when failure occurs. This paper proposed an active fault-Tolerant control (AFTC) strategy for civil aircraft with ailerons stuck at different degrees. The baseline control law was designed based on linear quadratic regulator (LQR) to guarantee lateral control stability and performance. On this basis, a reconfigurable controller was designed based on model reference for the supposed failures. The simulation of lateral motion under the numerical model of Boeing 747 was carried out with the consideration of the impact of spoilers. Comparing the simulation results under reconfigurable controller with AFTC strategy and only under basic controller, the AFTC strategy was proved to be effective precisely.

AB - As civil aircrafts require high requirement of reliability, the flight control system should make airplane safe at least when failure occurs. This paper proposed an active fault-Tolerant control (AFTC) strategy for civil aircraft with ailerons stuck at different degrees. The baseline control law was designed based on linear quadratic regulator (LQR) to guarantee lateral control stability and performance. On this basis, a reconfigurable controller was designed based on model reference for the supposed failures. The simulation of lateral motion under the numerical model of Boeing 747 was carried out with the consideration of the impact of spoilers. Comparing the simulation results under reconfigurable controller with AFTC strategy and only under basic controller, the AFTC strategy was proved to be effective precisely.

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M3 - 会议稿件

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PB - Institute of Electrical and Electronics Engineers Inc.

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Wang K, Wang S , Wang X, Yang Z. Active fault-Tolerant control strategy for lateral motion of civil aircraft. In AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems. Institute of Electrical and Electronics Engineers Inc. 2016. p. 713-718. 7748145. (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems). doi: 10.1109/AUS.2016.7748145

Active fault-Tolerant control strategy for lateral motion of civil aircraft

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