Adaptive turbulence compensation for aircraft flight control

Liyan Wen; Gang Tao; Hao Yang; Yanjun Zhang

doi:10.1109/CGNCC.2016.7829031

Adaptive turbulence compensation for aircraft flight control

Liyan Wen, Gang Tao, Hao Yang, Yanjun Zhang^*

^*Corresponding author for this work

Nanjing University of Aeronautics and Astronautics

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

Abstract

In this paper, a set of adaptive turbulence compensation techniques are investigated for aircraft flight control systems with different control gain matrices A(x), for which the multivariable adaptive disturbance rejection problems are formulated: one is for a nonsingular A(x), and one is for a singular A(x). Two unmatched disturbance rejection control design problems are addressed for the proposed aircraft turbulence compensation study: one with static feedback linearization under a direct control relative degree condition, and one with dynamic feedback linearization under an input extension control relative degree condition. For each problem, both nominal and adaptive turbulence compensation designs are developed for aircraft systems with known parameters and with unknown parameters, respectively. A typical aircraft application with turbulence disturbances is studied by a specific simulation study.

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	1612-1617
Number of pages	6
ISBN (Electronic)	9781467383189
DOIs	https://doi.org/10.1109/CGNCC.2016.7829031
Publication status	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

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10.1109/CGNCC.2016.7829031

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Wen, L., Tao, G., Yang, H., & Zhang, Y. (2017). Adaptive turbulence compensation for aircraft flight control. In CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference (pp. 1612-1617). Article 7829031 (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CGNCC.2016.7829031

@inproceedings{798125f142fc47d3b5dc3d80e394fa4a,

title = "Adaptive turbulence compensation for aircraft flight control",

abstract = "In this paper, a set of adaptive turbulence compensation techniques are investigated for aircraft flight control systems with different control gain matrices A(x), for which the multivariable adaptive disturbance rejection problems are formulated: one is for a nonsingular A(x), and one is for a singular A(x). Two unmatched disturbance rejection control design problems are addressed for the proposed aircraft turbulence compensation study: one with static feedback linearization under a direct control relative degree condition, and one with dynamic feedback linearization under an input extension control relative degree condition. For each problem, both nominal and adaptive turbulence compensation designs are developed for aircraft systems with known parameters and with unknown parameters, respectively. A typical aircraft application with turbulence disturbances is studied by a specific simulation study.",

author = "Liyan Wen and Gang Tao and Hao Yang and Yanjun 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.2016.7829031",

language = "English",

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

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

pages = "1612--1617",

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

address = "United States",

}

Wen, L, Tao, G, Yang, H & Zhang, Y 2017, Adaptive turbulence compensation for aircraft flight control. in CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference., 7829031, CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference, Institute of Electrical and Electronics Engineers Inc., pp. 1612-1617, 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016, Nanjing, Jiangsu, China, 12/08/16. https://doi.org/10.1109/CGNCC.2016.7829031

Adaptive turbulence compensation for aircraft flight control. / Wen, Liyan; Tao, Gang; Yang, Hao et al.
CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference. Institute of Electrical and Electronics Engineers Inc., 2017. p. 1612-1617 7829031 (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference).

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

TY - GEN

T1 - Adaptive turbulence compensation for aircraft flight control

AU - Wen, Liyan

AU - Tao, Gang

AU - Yang, Hao

AU - Zhang, Yanjun

PY - 2017/1/20

Y1 - 2017/1/20

N2 - In this paper, a set of adaptive turbulence compensation techniques are investigated for aircraft flight control systems with different control gain matrices A(x), for which the multivariable adaptive disturbance rejection problems are formulated: one is for a nonsingular A(x), and one is for a singular A(x). Two unmatched disturbance rejection control design problems are addressed for the proposed aircraft turbulence compensation study: one with static feedback linearization under a direct control relative degree condition, and one with dynamic feedback linearization under an input extension control relative degree condition. For each problem, both nominal and adaptive turbulence compensation designs are developed for aircraft systems with known parameters and with unknown parameters, respectively. A typical aircraft application with turbulence disturbances is studied by a specific simulation study.

AB - In this paper, a set of adaptive turbulence compensation techniques are investigated for aircraft flight control systems with different control gain matrices A(x), for which the multivariable adaptive disturbance rejection problems are formulated: one is for a nonsingular A(x), and one is for a singular A(x). Two unmatched disturbance rejection control design problems are addressed for the proposed aircraft turbulence compensation study: one with static feedback linearization under a direct control relative degree condition, and one with dynamic feedback linearization under an input extension control relative degree condition. For each problem, both nominal and adaptive turbulence compensation designs are developed for aircraft systems with known parameters and with unknown parameters, respectively. A typical aircraft application with turbulence disturbances is studied by a specific simulation study.

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U2 - 10.1109/CGNCC.2016.7829031

DO - 10.1109/CGNCC.2016.7829031

M3 - Conference contribution

AN - SCOPUS:85015147184

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

SP - 1612

EP - 1617

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 -

Adaptive turbulence compensation for aircraft flight control

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