Neural robust adaptive hypersonic flight control without back-stepping

Shixing Wang; Fuchun Sun; Yongquan Zhang; Bin Xu; Yiwei Zhang

doi:10.1109/CGNCC.2014.7007556

Neural robust adaptive hypersonic flight control without back-stepping

Shixing Wang
, Fuchun Sun
, Yongquan Zhang
, Bin Xu
, Yiwei Zhang

School of Automation

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

Abstract

In this paper, one robust adaptive controller is proposed for hypersonic flight dynamics with high gain observer (HGO) and neural networks (NNs). For the attitude subsystem, it contains flight path angle, pitch angle and pitch rate. To avoid the complex back-stepping design, the dynamics are transformed into the normal feedback form. With HGO estimating the newly defined states, the controller is proposed with error feedback, NN approximation and the robust item. It is proved that the NN weights and filtered tracking error are guaranteed in the semiglobal sense. The simulation with March 15 is conducted to show the effectiveness of the proposed method.

Original language	English
Title of host publication	2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	2468-2473
Number of pages	6
ISBN (Electronic)	9781479946990
DOIs	https://doi.org/10.1109/CGNCC.2014.7007556
State	Published - 12 Jan 2015
Event	6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 - Yantai, China Duration: 8 Aug 2014 → 10 Aug 2014

Publication series

Name	2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

Conference

Conference	6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
Country/Territory	China
City	Yantai
Period	8/08/14 → 10/08/14

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10.1109/CGNCC.2014.7007556

Cite this

Wang, S., Sun, F., Zhang, Y., Xu, B., & Zhang, Y. (2015). Neural robust adaptive hypersonic flight control without back-stepping. In 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 (pp. 2468-2473). Article 7007556 (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CGNCC.2014.7007556

@inproceedings{515dd6b030d8454784b035ea929da57f,

title = "Neural robust adaptive hypersonic flight control without back-stepping",

abstract = "In this paper, one robust adaptive controller is proposed for hypersonic flight dynamics with high gain observer (HGO) and neural networks (NNs). For the attitude subsystem, it contains flight path angle, pitch angle and pitch rate. To avoid the complex back-stepping design, the dynamics are transformed into the normal feedback form. With HGO estimating the newly defined states, the controller is proposed with error feedback, NN approximation and the robust item. It is proved that the NN weights and filtered tracking error are guaranteed in the semiglobal sense. The simulation with March 15 is conducted to show the effectiveness of the proposed method.",

author = "Shixing Wang and Fuchun Sun and Yongquan Zhang and Bin Xu and Yiwei Zhang",

note = "Publisher Copyright: {\textcopyright} 2014 IEEE.; 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 ; Conference date: 08-08-2014 Through 10-08-2014",

year = "2015",

month = jan,

day = "12",

doi = "10.1109/CGNCC.2014.7007556",

language = "英语",

series = "2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014",

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

pages = "2468--2473",

booktitle = "2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014",

}

Wang, S, Sun, F, Zhang, Y, Xu, B & Zhang, Y 2015, Neural robust adaptive hypersonic flight control without back-stepping. in 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014., 7007556, 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014, Institute of Electrical and Electronics Engineers Inc., pp. 2468-2473, 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014, Yantai, China, 8/08/14. https://doi.org/10.1109/CGNCC.2014.7007556

Neural robust adaptive hypersonic flight control without back-stepping. / Wang, Shixing; Sun, Fuchun; Zhang, Yongquan et al.
2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014. Institute of Electrical and Electronics Engineers Inc., 2015. p. 2468-2473 7007556 (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014).

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

TY - GEN

T1 - Neural robust adaptive hypersonic flight control without back-stepping

AU - Wang, Shixing

AU - Sun, Fuchun

AU - Zhang, Yongquan

AU - Xu, Bin

AU - Zhang, Yiwei

PY - 2015/1/12

Y1 - 2015/1/12

N2 - In this paper, one robust adaptive controller is proposed for hypersonic flight dynamics with high gain observer (HGO) and neural networks (NNs). For the attitude subsystem, it contains flight path angle, pitch angle and pitch rate. To avoid the complex back-stepping design, the dynamics are transformed into the normal feedback form. With HGO estimating the newly defined states, the controller is proposed with error feedback, NN approximation and the robust item. It is proved that the NN weights and filtered tracking error are guaranteed in the semiglobal sense. The simulation with March 15 is conducted to show the effectiveness of the proposed method.

AB - In this paper, one robust adaptive controller is proposed for hypersonic flight dynamics with high gain observer (HGO) and neural networks (NNs). For the attitude subsystem, it contains flight path angle, pitch angle and pitch rate. To avoid the complex back-stepping design, the dynamics are transformed into the normal feedback form. With HGO estimating the newly defined states, the controller is proposed with error feedback, NN approximation and the robust item. It is proved that the NN weights and filtered tracking error are guaranteed in the semiglobal sense. The simulation with March 15 is conducted to show the effectiveness of the proposed method.

UR - https://www.scopus.com/pages/publications/84922575251

U2 - 10.1109/CGNCC.2014.7007556

DO - 10.1109/CGNCC.2014.7007556

M3 - 会议稿件

AN - SCOPUS:84922575251

T3 - 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

SP - 2468

EP - 2473

BT - 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

Y2 - 8 August 2014 through 10 August 2014

ER -

Wang S, Sun F, Zhang Y, Xu B, Zhang Y. Neural robust adaptive hypersonic flight control without back-stepping. In 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014. Institute of Electrical and Electronics Engineers Inc. 2015. p. 2468-2473. 7007556. (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014). doi: 10.1109/CGNCC.2014.7007556

Neural robust adaptive hypersonic flight control without back-stepping

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