Robust continuous terminal sliding mode control design for a near-space hypersonic vehicle

Ruimin Zhang; Changyin Sun; Jingmei Zhang; Chengshan Qian

doi:10.1007/978-3-642-42057-3_87

Robust continuous terminal sliding mode control design for a near-space hypersonic vehicle

Ruimin Zhang
, Changyin Sun
, Jingmei Zhang
, Chengshan Qian

Southeast University, Nanjing
Henan University of Science and Technology

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

3 Scopus citations

Abstract

This paper presents a robust continuous terminal sliding mode attitude tracking control approach for a near-space hypersonic vehicle(NSHV) in the presence of parameter uncertainties and external disturbances. Firstly, a novel nonsingular terminal sliding surface is developed. Then, a continuous terminal sliding mode control law is proposed, which is chattering-free. Afterward, considering the presence of parameter uncertainties and external disturbances, a high order sliding mode disturbance observer is introduced to estimate the lumped disturbance to improve the control performance. Finally, numerical simulations applied to the NSHV illustrate the effectiveness of the proposed approach.

Original language	English
Title of host publication	Intelligence Science and Big Data Engineering - 4th International Conference, IScIDE 2013, Revised Selected Papers
Publisher	Springer Verlag
Pages	691-696
Number of pages	6
ISBN (Print)	9783642420566
DOIs	https://doi.org/10.1007/978-3-642-42057-3_87
State	Published - 2013
Externally published	Yes
Event	4th International Conference on Intelligence Science and Big Data Engineering, IScIDE 2013 - Beijing, China Duration: 31 Jul 2013 → 2 Aug 2013

Publication series

Name	Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)
Volume	8261 LNCS
ISSN (Print)	0302-9743
ISSN (Electronic)	1611-3349

Conference

Conference	4th International Conference on Intelligence Science and Big Data Engineering, IScIDE 2013
Country/Territory	China
City	Beijing
Period	31/07/13 → 2/08/13

Keywords

Finite-time convergence
Near-space hypersonic vehicle
Terminal sliding mode control
Tracking control

Access to Document

10.1007/978-3-642-42057-3_87

Cite this

Zhang, R., Sun, C., Zhang, J., & Qian, C. (2013). Robust continuous terminal sliding mode control design for a near-space hypersonic vehicle. In Intelligence Science and Big Data Engineering - 4th International Conference, IScIDE 2013, Revised Selected Papers (pp. 691-696). (Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics); Vol. 8261 LNCS). Springer Verlag. https://doi.org/10.1007/978-3-642-42057-3_87

Zhang, Ruimin ; Sun, Changyin ; Zhang, Jingmei et al. / Robust continuous terminal sliding mode control design for a near-space hypersonic vehicle. Intelligence Science and Big Data Engineering - 4th International Conference, IScIDE 2013, Revised Selected Papers. Springer Verlag, 2013. pp. 691-696 (Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)).

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title = "Robust continuous terminal sliding mode control design for a near-space hypersonic vehicle",

abstract = "This paper presents a robust continuous terminal sliding mode attitude tracking control approach for a near-space hypersonic vehicle(NSHV) in the presence of parameter uncertainties and external disturbances. Firstly, a novel nonsingular terminal sliding surface is developed. Then, a continuous terminal sliding mode control law is proposed, which is chattering-free. Afterward, considering the presence of parameter uncertainties and external disturbances, a high order sliding mode disturbance observer is introduced to estimate the lumped disturbance to improve the control performance. Finally, numerical simulations applied to the NSHV illustrate the effectiveness of the proposed approach.",

keywords = "Finite-time convergence, Near-space hypersonic vehicle, Terminal sliding mode control, Tracking control",

author = "Ruimin Zhang and Changyin Sun and Jingmei Zhang and Chengshan Qian",

year = "2013",

doi = "10.1007/978-3-642-42057-3\_87",

language = "英语",

isbn = "9783642420566",

series = "Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)",

publisher = "Springer Verlag",

pages = "691--696",

booktitle = "Intelligence Science and Big Data Engineering - 4th International Conference, IScIDE 2013, Revised Selected Papers",

note = "4th International Conference on Intelligence Science and Big Data Engineering, IScIDE 2013 ; Conference date: 31-07-2013 Through 02-08-2013",

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Zhang, R, Sun, C, Zhang, J & Qian, C 2013, Robust continuous terminal sliding mode control design for a near-space hypersonic vehicle. in Intelligence Science and Big Data Engineering - 4th International Conference, IScIDE 2013, Revised Selected Papers. Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics), vol. 8261 LNCS, Springer Verlag, pp. 691-696, 4th International Conference on Intelligence Science and Big Data Engineering, IScIDE 2013, Beijing, China, 31/07/13. https://doi.org/10.1007/978-3-642-42057-3_87

Robust continuous terminal sliding mode control design for a near-space hypersonic vehicle. / Zhang, Ruimin; Sun, Changyin; Zhang, Jingmei et al.
Intelligence Science and Big Data Engineering - 4th International Conference, IScIDE 2013, Revised Selected Papers. Springer Verlag, 2013. p. 691-696 (Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics); Vol. 8261 LNCS).

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

TY - GEN

T1 - Robust continuous terminal sliding mode control design for a near-space hypersonic vehicle

AU - Zhang, Ruimin

AU - Sun, Changyin

AU - Zhang, Jingmei

AU - Qian, Chengshan

PY - 2013

Y1 - 2013

N2 - This paper presents a robust continuous terminal sliding mode attitude tracking control approach for a near-space hypersonic vehicle(NSHV) in the presence of parameter uncertainties and external disturbances. Firstly, a novel nonsingular terminal sliding surface is developed. Then, a continuous terminal sliding mode control law is proposed, which is chattering-free. Afterward, considering the presence of parameter uncertainties and external disturbances, a high order sliding mode disturbance observer is introduced to estimate the lumped disturbance to improve the control performance. Finally, numerical simulations applied to the NSHV illustrate the effectiveness of the proposed approach.

AB - This paper presents a robust continuous terminal sliding mode attitude tracking control approach for a near-space hypersonic vehicle(NSHV) in the presence of parameter uncertainties and external disturbances. Firstly, a novel nonsingular terminal sliding surface is developed. Then, a continuous terminal sliding mode control law is proposed, which is chattering-free. Afterward, considering the presence of parameter uncertainties and external disturbances, a high order sliding mode disturbance observer is introduced to estimate the lumped disturbance to improve the control performance. Finally, numerical simulations applied to the NSHV illustrate the effectiveness of the proposed approach.

KW - Finite-time convergence

KW - Near-space hypersonic vehicle

KW - Terminal sliding mode control

KW - Tracking control

UR - https://www.scopus.com/pages/publications/84892857022

U2 - 10.1007/978-3-642-42057-3_87

DO - 10.1007/978-3-642-42057-3_87

M3 - 会议稿件

AN - SCOPUS:84892857022

SN - 9783642420566

T3 - Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)

SP - 691

EP - 696

BT - Intelligence Science and Big Data Engineering - 4th International Conference, IScIDE 2013, Revised Selected Papers

PB - Springer Verlag

T2 - 4th International Conference on Intelligence Science and Big Data Engineering, IScIDE 2013

Y2 - 31 July 2013 through 2 August 2013

ER -

Zhang R, Sun C, Zhang J, Qian C. Robust continuous terminal sliding mode control design for a near-space hypersonic vehicle. In Intelligence Science and Big Data Engineering - 4th International Conference, IScIDE 2013, Revised Selected Papers. Springer Verlag. 2013. p. 691-696. (Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)). doi: 10.1007/978-3-642-42057-3_87

Robust continuous terminal sliding mode control design for a near-space hypersonic vehicle

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