Nonlinear characteristic model-based SMC and its application to flexible satellites

L. Chen; Y. Yan; C. Y. Sun

doi:10.3182/20140824-6-za-1003.01200

Nonlinear characteristic model-based SMC and its application to flexible satellites

L. Chen, Y. Yan, C. Y. Sun

Southeast University, Nanjing

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

6 Citations (Scopus)

Abstract

This study investigates the sliding mode control (SMC) method based on the nonlinear characteristic model and its application to flexible satellites. A novel nonlinear dynamic sliding mode surface is designed depending on the nonlinear characteristic model. The expected advantage of the proposed SMC compared to the traditional SMC is to improve performances and robustness. The proposed results apply to a class of nonlinear systems and rely on the parameter estimation of the characteristic model. The theory is illustrated on the rapid maneuver and fast stability problem of the sun synchronous orbit satellite.

Original language	English
Title of host publication	19th IFAC World Congress IFAC 2014, Proceedings
Editors	Edward Boje, Xiaohua Xia
Publisher	IFAC Secretariat
Pages	4595-4600
Number of pages	6
ISBN (Electronic)	9783902823625
DOIs	https://doi.org/10.3182/20140824-6-za-1003.01200
Publication status	Published - 2014
Externally published	Yes
Event	19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014 - Cape Town, South Africa Duration: 24 Aug 2014 → 29 Aug 2014

Publication series

Name	IFAC Proceedings Volumes (IFAC-PapersOnline)
Volume	19
ISSN (Print)	1474-6670

Conference

Conference	19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014
Country/Territory	South Africa
City	Cape Town
Period	24/08/14 → 29/08/14

Keywords

Characteristic model
Flexible satellite
Rapid maneuver
Sliding mode control

Access to Document

10.3182/20140824-6-za-1003.01200

Cite this

Chen, L., Yan, Y., & Sun, C. Y. (2014). Nonlinear characteristic model-based SMC and its application to flexible satellites. In E. Boje, & X. Xia (Eds.), 19th IFAC World Congress IFAC 2014, Proceedings (pp. 4595-4600). (IFAC Proceedings Volumes (IFAC-PapersOnline); Vol. 19). IFAC Secretariat. https://doi.org/10.3182/20140824-6-za-1003.01200

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title = "Nonlinear characteristic model-based SMC and its application to flexible satellites",

abstract = "This study investigates the sliding mode control (SMC) method based on the nonlinear characteristic model and its application to flexible satellites. A novel nonlinear dynamic sliding mode surface is designed depending on the nonlinear characteristic model. The expected advantage of the proposed SMC compared to the traditional SMC is to improve performances and robustness. The proposed results apply to a class of nonlinear systems and rely on the parameter estimation of the characteristic model. The theory is illustrated on the rapid maneuver and fast stability problem of the sun synchronous orbit satellite.",

keywords = "Characteristic model, Flexible satellite, Rapid maneuver, Sliding mode control",

author = "L. Chen and Y. Yan and Sun, {C. Y.}",

note = "Publisher Copyright: {\textcopyright} IFAC.; 19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014 ; Conference date: 24-08-2014 Through 29-08-2014",

year = "2014",

doi = "10.3182/20140824-6-za-1003.01200",

language = "English",

series = "IFAC Proceedings Volumes (IFAC-PapersOnline)",

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booktitle = "19th IFAC World Congress IFAC 2014, Proceedings",

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Chen, L, Yan, Y & Sun, CY 2014, Nonlinear characteristic model-based SMC and its application to flexible satellites. in E Boje & X Xia (eds), 19th IFAC World Congress IFAC 2014, Proceedings. IFAC Proceedings Volumes (IFAC-PapersOnline), vol. 19, IFAC Secretariat, pp. 4595-4600, 19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014, Cape Town, South Africa, 24/08/14. https://doi.org/10.3182/20140824-6-za-1003.01200

Nonlinear characteristic model-based SMC and its application to flexible satellites. / Chen, L.; Yan, Y.; Sun, C. Y.
19th IFAC World Congress IFAC 2014, Proceedings. ed. / Edward Boje; Xiaohua Xia. IFAC Secretariat, 2014. p. 4595-4600 (IFAC Proceedings Volumes (IFAC-PapersOnline); Vol. 19).

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

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T1 - Nonlinear characteristic model-based SMC and its application to flexible satellites

AU - Chen, L.

AU - Yan, Y.

AU - Sun, C. Y.

N1 - Publisher Copyright: © IFAC.

PY - 2014

Y1 - 2014

N2 - This study investigates the sliding mode control (SMC) method based on the nonlinear characteristic model and its application to flexible satellites. A novel nonlinear dynamic sliding mode surface is designed depending on the nonlinear characteristic model. The expected advantage of the proposed SMC compared to the traditional SMC is to improve performances and robustness. The proposed results apply to a class of nonlinear systems and rely on the parameter estimation of the characteristic model. The theory is illustrated on the rapid maneuver and fast stability problem of the sun synchronous orbit satellite.

AB - This study investigates the sliding mode control (SMC) method based on the nonlinear characteristic model and its application to flexible satellites. A novel nonlinear dynamic sliding mode surface is designed depending on the nonlinear characteristic model. The expected advantage of the proposed SMC compared to the traditional SMC is to improve performances and robustness. The proposed results apply to a class of nonlinear systems and rely on the parameter estimation of the characteristic model. The theory is illustrated on the rapid maneuver and fast stability problem of the sun synchronous orbit satellite.

KW - Characteristic model

KW - Flexible satellite

KW - Rapid maneuver

KW - Sliding mode control

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DO - 10.3182/20140824-6-za-1003.01200

M3 - Conference contribution

AN - SCOPUS:84929718698

T3 - IFAC Proceedings Volumes (IFAC-PapersOnline)

SP - 4595

EP - 4600

BT - 19th IFAC World Congress IFAC 2014, Proceedings

A2 - Boje, Edward

A2 - Xia, Xiaohua

PB - IFAC Secretariat

T2 - 19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014

Y2 - 24 August 2014 through 29 August 2014

ER -

Nonlinear characteristic model-based SMC and its application to flexible satellites

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Keywords

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