Journal article 804 views
Global Neural Dynamic Surface Tracking Control of Strict-Feedback Systems With Application to Hypersonic Flight Vehicle
IEEE Transactions on Neural Networks and Learning Systems, Volume: 26, Issue: 10, Pages: 2563 - 2575
Swansea University Author: Chenguang Yang
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DOI (Published version): 10.1109/TNNLS.2015.2456972
Abstract
In this paper, we investigate both indirect and direct global neural control of nonlinear systems in strict-feedback form. The dynamic surface control (DSC) technique is employed together with a novel switching mechanism, and neural approximation is utilized to compensate for the effect caused by un...
Published in: | IEEE Transactions on Neural Networks and Learning Systems |
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2015
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URI: | https://cronfa.swan.ac.uk/Record/cronfa27024 |
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2016-04-02T01:02:49Z |
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2021-10-21T02:44:29Z |
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2021-10-20T10:56:04.4977372 v2 27024 2016-04-01 Global Neural Dynamic Surface Tracking Control of Strict-Feedback Systems With Application to Hypersonic Flight Vehicle d2a5024448bfac00a9b3890a8404380b Chenguang Yang Chenguang Yang true false 2016-04-01 In this paper, we investigate both indirect and direct global neural control of nonlinear systems in strict-feedback form. The dynamic surface control (DSC) technique is employed together with a novel switching mechanism, and neural approximation is utilized to compensate for the effect caused by unknown dynamics. A robust term is integrated into the control design to pull the transient states back into the neural approximation domain when they go beyond. The proposed method ensures globally uniformly ultimately boundedness stability, in comparison to the conventional semiglobal stability achieved by most existing neural controllers. Simulation studies are performed on a hypersonic flight vehicle (HFV) model to verify the effectiveness of the proposed global neural controller. Journal Article IEEE Transactions on Neural Networks and Learning Systems 26 10 2563 2575 31 10 2015 2015-10-31 10.1109/TNNLS.2015.2456972 COLLEGE NANME COLLEGE CODE Swansea University 2021-10-20T10:56:04.4977372 2016-04-01T17:33:21.4205802 Faculty of Science and Engineering School of Engineering and Applied Sciences - Uncategorised Bin Xu 1 Chenguang Yang 2 Yongping Pan 3 |
title |
Global Neural Dynamic Surface Tracking Control of Strict-Feedback Systems With Application to Hypersonic Flight Vehicle |
spellingShingle |
Global Neural Dynamic Surface Tracking Control of Strict-Feedback Systems With Application to Hypersonic Flight Vehicle Chenguang Yang |
title_short |
Global Neural Dynamic Surface Tracking Control of Strict-Feedback Systems With Application to Hypersonic Flight Vehicle |
title_full |
Global Neural Dynamic Surface Tracking Control of Strict-Feedback Systems With Application to Hypersonic Flight Vehicle |
title_fullStr |
Global Neural Dynamic Surface Tracking Control of Strict-Feedback Systems With Application to Hypersonic Flight Vehicle |
title_full_unstemmed |
Global Neural Dynamic Surface Tracking Control of Strict-Feedback Systems With Application to Hypersonic Flight Vehicle |
title_sort |
Global Neural Dynamic Surface Tracking Control of Strict-Feedback Systems With Application to Hypersonic Flight Vehicle |
author_id_str_mv |
d2a5024448bfac00a9b3890a8404380b |
author_id_fullname_str_mv |
d2a5024448bfac00a9b3890a8404380b_***_Chenguang Yang |
author |
Chenguang Yang |
author2 |
Bin Xu Chenguang Yang Yongping Pan |
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IEEE Transactions on Neural Networks and Learning Systems |
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2563 |
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2015 |
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Swansea University |
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10.1109/TNNLS.2015.2456972 |
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Faculty of Science and Engineering |
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Faculty of Science and Engineering |
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facultyofscienceandengineering |
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Faculty of Science and Engineering |
department_str |
School of Engineering and Applied Sciences - Uncategorised{{{_:::_}}}Faculty of Science and Engineering{{{_:::_}}}School of Engineering and Applied Sciences - Uncategorised |
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description |
In this paper, we investigate both indirect and direct global neural control of nonlinear systems in strict-feedback form. The dynamic surface control (DSC) technique is employed together with a novel switching mechanism, and neural approximation is utilized to compensate for the effect caused by unknown dynamics. A robust term is integrated into the control design to pull the transient states back into the neural approximation domain when they go beyond. The proposed method ensures globally uniformly ultimately boundedness stability, in comparison to the conventional semiglobal stability achieved by most existing neural controllers. Simulation studies are performed on a hypersonic flight vehicle (HFV) model to verify the effectiveness of the proposed global neural controller. |
published_date |
2015-10-31T12:58:20Z |
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1821410381407453184 |
score |
11.048237 |