Fault tolerant control for vertical tail damaged Aircraft in final approach with switching LQR controller

Zhangtao Wang; Shaoping Wang; Xingjian Wang

doi:10.1109/ICIEA.2017.8282823

Fault tolerant control for vertical tail damaged Aircraft in final approach with switching LQR controller

Zhangtao Wang
, Shaoping Wang
, Xingjian Wang

School of Automation Science and Electrical Engineering

Beihang University

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

4 Scopus citations

Abstract

This paper mainly focus on the fault tolerant control issue of vertical tail damaged aircrafts during landing process in final approach. A damage indicator is used to describe the damage degree of the vertical tail and rudder. Based on the damage indicator, the nonlinear relationship between the damage degree indicator and corresponding aerodynamic stability derivatives is fully considered. Nonlinear relationship between rudder derivative, vertical tail derivative and damage indicator in different low Mach number situations were studied. Furthermore, a modified state space feedback controller with variable element linear quadratic regulator (LQR) is proposed for changing objective between different control variables in different stages of final approach.

Original language	English
Title of host publication	Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	105-109
Number of pages	5
ISBN (Electronic)	9781538621035
DOIs	https://doi.org/10.1109/ICIEA.2017.8282823
State	Published - 2 Jul 2017
Event	12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017 - Siem Reap, Cambodia Duration: 18 Jun 2017 → 20 Jun 2017

Publication series

Name	Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017
Volume	2018-February

Conference

Conference	12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017
Country/Territory	Cambodia
City	Siem Reap
Period	18/06/17 → 20/06/17

Keywords

Fault tolerant control
final approach
linear quadratic regulator
state space feedback control
vertical tail damage

Access to Document

10.1109/ICIEA.2017.8282823

Cite this

Wang, Z., Wang, S., & Wang, X. (2017). Fault tolerant control for vertical tail damaged Aircraft in final approach with switching LQR controller. In Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017 (pp. 105-109). (Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017; Vol. 2018-February). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICIEA.2017.8282823

Wang, Zhangtao ; Wang, Shaoping ; Wang, Xingjian. / Fault tolerant control for vertical tail damaged Aircraft in final approach with switching LQR controller. Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017. Institute of Electrical and Electronics Engineers Inc., 2017. pp. 105-109 (Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017).

@inproceedings{d21d3b2d11d348fcade6345c8cdfd4b2,

title = "Fault tolerant control for vertical tail damaged Aircraft in final approach with switching LQR controller",

abstract = "This paper mainly focus on the fault tolerant control issue of vertical tail damaged aircrafts during landing process in final approach. A damage indicator is used to describe the damage degree of the vertical tail and rudder. Based on the damage indicator, the nonlinear relationship between the damage degree indicator and corresponding aerodynamic stability derivatives is fully considered. Nonlinear relationship between rudder derivative, vertical tail derivative and damage indicator in different low Mach number situations were studied. Furthermore, a modified state space feedback controller with variable element linear quadratic regulator (LQR) is proposed for changing objective between different control variables in different stages of final approach.",

keywords = "Fault tolerant control, final approach, linear quadratic regulator, state space feedback control, vertical tail damage",

author = "Zhangtao Wang and Shaoping Wang and Xingjian Wang",

note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017 ; Conference date: 18-06-2017 Through 20-06-2017",

year = "2017",

month = jul,

day = "2",

doi = "10.1109/ICIEA.2017.8282823",

language = "英语",

series = "Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017",

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

pages = "105--109",

booktitle = "Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017",

address = "美国",

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Wang, Z, Wang, S & Wang, X 2017, Fault tolerant control for vertical tail damaged Aircraft in final approach with switching LQR controller. in Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017. Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017, vol. 2018-February, Institute of Electrical and Electronics Engineers Inc., pp. 105-109, 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017, Siem Reap, Cambodia, 18/06/17. https://doi.org/10.1109/ICIEA.2017.8282823

Fault tolerant control for vertical tail damaged Aircraft in final approach with switching LQR controller. / Wang, Zhangtao; Wang, Shaoping ; Wang, Xingjian.
Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017. Institute of Electrical and Electronics Engineers Inc., 2017. p. 105-109 (Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017; Vol. 2018-February).

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

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AU - Wang, Zhangtao

AU - Wang, Shaoping

AU - Wang, Xingjian

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N2 - This paper mainly focus on the fault tolerant control issue of vertical tail damaged aircrafts during landing process in final approach. A damage indicator is used to describe the damage degree of the vertical tail and rudder. Based on the damage indicator, the nonlinear relationship between the damage degree indicator and corresponding aerodynamic stability derivatives is fully considered. Nonlinear relationship between rudder derivative, vertical tail derivative and damage indicator in different low Mach number situations were studied. Furthermore, a modified state space feedback controller with variable element linear quadratic regulator (LQR) is proposed for changing objective between different control variables in different stages of final approach.

AB - This paper mainly focus on the fault tolerant control issue of vertical tail damaged aircrafts during landing process in final approach. A damage indicator is used to describe the damage degree of the vertical tail and rudder. Based on the damage indicator, the nonlinear relationship between the damage degree indicator and corresponding aerodynamic stability derivatives is fully considered. Nonlinear relationship between rudder derivative, vertical tail derivative and damage indicator in different low Mach number situations were studied. Furthermore, a modified state space feedback controller with variable element linear quadratic regulator (LQR) is proposed for changing objective between different control variables in different stages of final approach.

KW - Fault tolerant control

KW - final approach

KW - linear quadratic regulator

KW - state space feedback control

KW - vertical tail damage

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DO - 10.1109/ICIEA.2017.8282823

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BT - Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017

PB - Institute of Electrical and Electronics Engineers Inc.

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Wang Z, Wang S , Wang X. Fault tolerant control for vertical tail damaged Aircraft in final approach with switching LQR controller. In Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017. Institute of Electrical and Electronics Engineers Inc. 2017. p. 105-109. (Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017). doi: 10.1109/ICIEA.2017.8282823

Fault tolerant control for vertical tail damaged Aircraft in final approach with switching LQR controller

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