Robust Neural Direct Hypersonic Flight Control Under Actuator Saturation

Xia Wang; Bin Xu; Pengchao Zhang; Yu Zhang

doi:10.1007/978-981-13-7986-4_36

Robust Neural Direct Hypersonic Flight Control Under Actuator Saturation

Xia Wang, Bin Xu, Pengchao Zhang, Yu Zhang

School of Automation

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

Abstract

This work addresses the robust neural direct control of hypersonics flight vehicle (HFV) under dynamics uncertainty and actuator saturation. The controller is constructed with robust control and neural control. To deal with the actuator saturation, a Gaussian error function is employed to express the effect. The dynamic surface control (DSC) is studied to remove the explosion of the complexity by using a nonlinear adaptive filter. The simulation tested on the hypersonic vehicle control-oriented model (COM) shows the effectiveness of the control design.

Original language	English
Title of host publication	Cognitive Systems and Signal Processing - 4th International Conference, ICCSIP 2018, Revised Selected Papers
Editors	Dewen Hu, Fuchun Sun, Huaping Liu
Publisher	Springer Verlag
Pages	406-414
Number of pages	9
ISBN (Print)	9789811379857
DOIs	https://doi.org/10.1007/978-981-13-7986-4_36
State	Published - 2019
Event	4th International Conference on Cognitive Systems and Information Processing, ICCSIP 2018 - Beijing, China Duration: 29 Nov 2018 → 1 Dec 2018

Publication series

Name	Communications in Computer and Information Science
Volume	1006
ISSN (Print)	1865-0929
ISSN (Electronic)	1865-0937

Conference

Conference	4th International Conference on Cognitive Systems and Information Processing, ICCSIP 2018
Country/Territory	China
City	Beijing
Period	29/11/18 → 1/12/18

Keywords

Actuator saturation
Hypersonic flight vehicle
Neural network (NN)

Access to Document

10.1007/978-981-13-7986-4_36

Cite this

Wang, X., Xu, B., Zhang, P., & Zhang, Y. (2019). Robust Neural Direct Hypersonic Flight Control Under Actuator Saturation. In D. Hu, F. Sun, & H. Liu (Eds.), Cognitive Systems and Signal Processing - 4th International Conference, ICCSIP 2018, Revised Selected Papers (pp. 406-414). (Communications in Computer and Information Science; Vol. 1006). Springer Verlag. https://doi.org/10.1007/978-981-13-7986-4_36

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title = "Robust Neural Direct Hypersonic Flight Control Under Actuator Saturation",

abstract = "This work addresses the robust neural direct control of hypersonics flight vehicle (HFV) under dynamics uncertainty and actuator saturation. The controller is constructed with robust control and neural control. To deal with the actuator saturation, a Gaussian error function is employed to express the effect. The dynamic surface control (DSC) is studied to remove the explosion of the complexity by using a nonlinear adaptive filter. The simulation tested on the hypersonic vehicle control-oriented model (COM) shows the effectiveness of the control design.",

keywords = "Actuator saturation, Hypersonic flight vehicle, Neural network (NN)",

author = "Xia Wang and Bin Xu and Pengchao Zhang and Yu Zhang",

note = "Publisher Copyright: © 2019, Springer Nature Singapore Pte Ltd.; 4th International Conference on Cognitive Systems and Information Processing, ICCSIP 2018 ; Conference date: 29-11-2018 Through 01-12-2018",

year = "2019",

doi = "10.1007/978-981-13-7986-4_36",

language = "英语",

isbn = "9789811379857",

series = "Communications in Computer and Information Science",

publisher = "Springer Verlag",

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editor = "Dewen Hu and Fuchun Sun and Huaping Liu",

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Wang, X, Xu, B, Zhang, P & Zhang, Y 2019, Robust Neural Direct Hypersonic Flight Control Under Actuator Saturation. in D Hu, F Sun & H Liu (eds), Cognitive Systems and Signal Processing - 4th International Conference, ICCSIP 2018, Revised Selected Papers. Communications in Computer and Information Science, vol. 1006, Springer Verlag, pp. 406-414, 4th International Conference on Cognitive Systems and Information Processing, ICCSIP 2018, Beijing, China, 29/11/18. https://doi.org/10.1007/978-981-13-7986-4_36

Robust Neural Direct Hypersonic Flight Control Under Actuator Saturation. / Wang, Xia; Xu, Bin; Zhang, Pengchao et al.
Cognitive Systems and Signal Processing - 4th International Conference, ICCSIP 2018, Revised Selected Papers. ed. / Dewen Hu; Fuchun Sun; Huaping Liu. Springer Verlag, 2019. p. 406-414 (Communications in Computer and Information Science; Vol. 1006).

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

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N2 - This work addresses the robust neural direct control of hypersonics flight vehicle (HFV) under dynamics uncertainty and actuator saturation. The controller is constructed with robust control and neural control. To deal with the actuator saturation, a Gaussian error function is employed to express the effect. The dynamic surface control (DSC) is studied to remove the explosion of the complexity by using a nonlinear adaptive filter. The simulation tested on the hypersonic vehicle control-oriented model (COM) shows the effectiveness of the control design.

AB - This work addresses the robust neural direct control of hypersonics flight vehicle (HFV) under dynamics uncertainty and actuator saturation. The controller is constructed with robust control and neural control. To deal with the actuator saturation, a Gaussian error function is employed to express the effect. The dynamic surface control (DSC) is studied to remove the explosion of the complexity by using a nonlinear adaptive filter. The simulation tested on the hypersonic vehicle control-oriented model (COM) shows the effectiveness of the control design.

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Wang X, Xu B, Zhang P, Zhang Y. Robust Neural Direct Hypersonic Flight Control Under Actuator Saturation. In Hu D, Sun F, Liu H, editors, Cognitive Systems and Signal Processing - 4th International Conference, ICCSIP 2018, Revised Selected Papers. Springer Verlag. 2019. p. 406-414. (Communications in Computer and Information Science). doi: 10.1007/978-981-13-7986-4_36

Robust Neural Direct Hypersonic Flight Control Under Actuator Saturation

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