Adaptive Control with Pseudo-Control Hedging for a Hypersonic Air Vehicle

Weixiong Lu; Qingzhen Zhang; Kun Ni; Song Ye

doi:10.1109/CGNCC.2016.7828815

Adaptive Control with Pseudo-Control Hedging for a Hypersonic Air Vehicle

Weixiong Lu^*
, Qingzhen Zhang
, Kun Ni
, Song Ye

^*此作品的通讯作者

自动化科学与电气工程学院

Beihang University

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

摘要

For an air-breathing Hypersonic Air Vehicle (HAV) in cruise flight, the model is strongly nonlinear and coupled and includes uncertain parameters. A pseudo-linear model is obtained by input/output feedback linearization, and a model reference adaptive controller is applied to it. Single Hidden Layer (SHL) Perceptron Neural Network (NN) is used to cancel model error online because of its good nonlinear approximation. Considering that large-span maneuver or strong disturbance can cause control surface saturation, Pseudo-Control Hedging (PCH) is introduced. Simulation results show that the proposed adaptive control system has well tracking performance, strong robustness and anti-input-saturation characteristics.

源语言	英语
主期刊名	CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
出版商	Institute of Electrical and Electronics Engineers Inc.
页	379-384
页数	6
ISBN（电子版）	9781467383189
DOI	https://doi.org/10.1109/CGNCC.2016.7828815
出版状态	已出版 - 20 1月 2017
活动	7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016 - Nanjing, Jiangsu, 中国期限: 12 8月 2016 → 14 8月 2016

出版系列

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

会议

会议	7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016
国家/地区	中国
市	Nanjing, Jiangsu
时期	12/08/16 → 14/08/16

访问文件

10.1109/CGNCC.2016.7828815

其它文件与链接

链接到 Scopus 的出版物

引用此

Lu, W., Zhang, Q., Ni, K., & Ye, S. (2017). Adaptive Control with Pseudo-Control Hedging for a Hypersonic Air Vehicle. 在 CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference (页码 379-384). 文章 7828815 (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CGNCC.2016.7828815

@inproceedings{2854f4cfa14d4c479bc68d5dddd7eef1,

title = "Adaptive Control with Pseudo-Control Hedging for a Hypersonic Air Vehicle",

abstract = "For an air-breathing Hypersonic Air Vehicle (HAV) in cruise flight, the model is strongly nonlinear and coupled and includes uncertain parameters. A pseudo-linear model is obtained by input/output feedback linearization, and a model reference adaptive controller is applied to it. Single Hidden Layer (SHL) Perceptron Neural Network (NN) is used to cancel model error online because of its good nonlinear approximation. Considering that large-span maneuver or strong disturbance can cause control surface saturation, Pseudo-Control Hedging (PCH) is introduced. Simulation results show that the proposed adaptive control system has well tracking performance, strong robustness and anti-input-saturation characteristics.",

author = "Weixiong Lu and Qingzhen Zhang and Kun Ni and Song Ye",

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.2016.7828815",

language = "英语",

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

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

pages = "379--384",

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

address = "美国",

}

Lu, W, Zhang, Q, Ni, K & Ye, S 2017, Adaptive Control with Pseudo-Control Hedging for a Hypersonic Air Vehicle. 在 CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference., 7828815, CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference, Institute of Electrical and Electronics Engineers Inc., 页码 379-384, 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016, Nanjing, Jiangsu, 中国, 12/08/16. https://doi.org/10.1109/CGNCC.2016.7828815

Adaptive Control with Pseudo-Control Hedging for a Hypersonic Air Vehicle. / Lu, Weixiong; Zhang, Qingzhen; Ni, Kun 等.
CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference. Institute of Electrical and Electronics Engineers Inc., 2017. 页码 379-384 7828815 (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

TY - GEN

T1 - Adaptive Control with Pseudo-Control Hedging for a Hypersonic Air Vehicle

AU - Lu, Weixiong

AU - Zhang, Qingzhen

AU - Ni, Kun

AU - Ye, Song

PY - 2017/1/20

Y1 - 2017/1/20

N2 - For an air-breathing Hypersonic Air Vehicle (HAV) in cruise flight, the model is strongly nonlinear and coupled and includes uncertain parameters. A pseudo-linear model is obtained by input/output feedback linearization, and a model reference adaptive controller is applied to it. Single Hidden Layer (SHL) Perceptron Neural Network (NN) is used to cancel model error online because of its good nonlinear approximation. Considering that large-span maneuver or strong disturbance can cause control surface saturation, Pseudo-Control Hedging (PCH) is introduced. Simulation results show that the proposed adaptive control system has well tracking performance, strong robustness and anti-input-saturation characteristics.

AB - For an air-breathing Hypersonic Air Vehicle (HAV) in cruise flight, the model is strongly nonlinear and coupled and includes uncertain parameters. A pseudo-linear model is obtained by input/output feedback linearization, and a model reference adaptive controller is applied to it. Single Hidden Layer (SHL) Perceptron Neural Network (NN) is used to cancel model error online because of its good nonlinear approximation. Considering that large-span maneuver or strong disturbance can cause control surface saturation, Pseudo-Control Hedging (PCH) is introduced. Simulation results show that the proposed adaptive control system has well tracking performance, strong robustness and anti-input-saturation characteristics.

UR - https://www.scopus.com/pages/publications/85015212150

U2 - 10.1109/CGNCC.2016.7828815

DO - 10.1109/CGNCC.2016.7828815

M3 - 会议稿件

AN - SCOPUS:85015212150

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

SP - 379

EP - 384

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 -

Lu W, Zhang Q, Ni K, Ye S. Adaptive Control with Pseudo-Control Hedging for a Hypersonic Air Vehicle. 在 CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference. Institute of Electrical and Electronics Engineers Inc. 2017. 页码 379-384. 7828815. (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference). doi: 10.1109/CGNCC.2016.7828815

Adaptive Control with Pseudo-Control Hedging for a Hypersonic Air Vehicle

摘要

出版系列

会议

访问文件

其它文件与链接

指纹

引用此