Finite time integral sliding mode control of hypersonic vehicles
Abstract This study investigates the tracking control problem for the longitudinal model of an airbreathing hypersonic vehicle (AHV) with external disturbances. By introducing finite time integral sliding mode manifolds, a novel finite time control method is designed for the longitudinal model of an...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Sun, Haibin [verfasserIn] |
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| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2013 |
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| Schlagwörter: |
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| Anmerkung: |
© Springer Science+Business Media Dordrecht 2013 |
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| Übergeordnetes Werk: |
Enthalten in: Nonlinear dynamics - Springer Netherlands, 1990, 73(2013), 1-2 vom: 30. Jan., Seite 229-244 |
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| Übergeordnetes Werk: |
volume:73 ; year:2013 ; number:1-2 ; day:30 ; month:01 ; pages:229-244 |
| Links: |
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| DOI / URN: |
10.1007/s11071-013-0780-4 |
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| Katalog-ID: |
OLC2051098115 |
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| 520 | |a Abstract This study investigates the tracking control problem for the longitudinal model of an airbreathing hypersonic vehicle (AHV) with external disturbances. By introducing finite time integral sliding mode manifolds, a novel finite time control method is designed for the longitudinal model of an AHV. This control method makes the velocity and altitude track the reference signals in finite time. Meanwhile, considering the large chattering phenomenon caused by high switching gains, an improved sliding mode control method based on nonlinear disturbance observer is proposed to reduce chattering. Through disturbance estimation for feedforward compensation, the improved sliding mode controller may take a smaller value for the switching gain without sacrificing disturbance rejection performance. Simulation results are provided to confirm the effectiveness of the proposed approach. | ||
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| 700 | 1 | |a Sun, Changyin |4 aut | |
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10.1007/s11071-013-0780-4 doi (DE-627)OLC2051098115 (DE-He213)s11071-013-0780-4-p DE-627 ger DE-627 rakwb eng 510 VZ 11 ssgn Sun, Haibin verfasserin aut Finite time integral sliding mode control of hypersonic vehicles 2013 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media Dordrecht 2013 Abstract This study investigates the tracking control problem for the longitudinal model of an airbreathing hypersonic vehicle (AHV) with external disturbances. By introducing finite time integral sliding mode manifolds, a novel finite time control method is designed for the longitudinal model of an AHV. This control method makes the velocity and altitude track the reference signals in finite time. Meanwhile, considering the large chattering phenomenon caused by high switching gains, an improved sliding mode control method based on nonlinear disturbance observer is proposed to reduce chattering. Through disturbance estimation for feedforward compensation, the improved sliding mode controller may take a smaller value for the switching gain without sacrificing disturbance rejection performance. Simulation results are provided to confirm the effectiveness of the proposed approach. Airbreathing hypersonic vehicle Sliding mode control Finite time stability Nonlinear disturbance observer Li, Shihua aut Sun, Changyin aut Enthalten in Nonlinear dynamics Springer Netherlands, 1990 73(2013), 1-2 vom: 30. Jan., Seite 229-244 (DE-627)130936782 (DE-600)1058624-6 (DE-576)034188126 0924-090X nnns volume:73 year:2013 number:1-2 day:30 month:01 pages:229-244 https://doi.org/10.1007/s11071-013-0780-4 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY SSG-OLC-CHE SSG-OLC-MAT SSG-OPC-MAT GBV_ILN_70 AR 73 2013 1-2 30 01 229-244 |
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10.1007/s11071-013-0780-4 doi (DE-627)OLC2051098115 (DE-He213)s11071-013-0780-4-p DE-627 ger DE-627 rakwb eng 510 VZ 11 ssgn Sun, Haibin verfasserin aut Finite time integral sliding mode control of hypersonic vehicles 2013 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media Dordrecht 2013 Abstract This study investigates the tracking control problem for the longitudinal model of an airbreathing hypersonic vehicle (AHV) with external disturbances. By introducing finite time integral sliding mode manifolds, a novel finite time control method is designed for the longitudinal model of an AHV. This control method makes the velocity and altitude track the reference signals in finite time. Meanwhile, considering the large chattering phenomenon caused by high switching gains, an improved sliding mode control method based on nonlinear disturbance observer is proposed to reduce chattering. Through disturbance estimation for feedforward compensation, the improved sliding mode controller may take a smaller value for the switching gain without sacrificing disturbance rejection performance. Simulation results are provided to confirm the effectiveness of the proposed approach. Airbreathing hypersonic vehicle Sliding mode control Finite time stability Nonlinear disturbance observer Li, Shihua aut Sun, Changyin aut Enthalten in Nonlinear dynamics Springer Netherlands, 1990 73(2013), 1-2 vom: 30. Jan., Seite 229-244 (DE-627)130936782 (DE-600)1058624-6 (DE-576)034188126 0924-090X nnns volume:73 year:2013 number:1-2 day:30 month:01 pages:229-244 https://doi.org/10.1007/s11071-013-0780-4 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY SSG-OLC-CHE SSG-OLC-MAT SSG-OPC-MAT GBV_ILN_70 AR 73 2013 1-2 30 01 229-244 |
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10.1007/s11071-013-0780-4 doi (DE-627)OLC2051098115 (DE-He213)s11071-013-0780-4-p DE-627 ger DE-627 rakwb eng 510 VZ 11 ssgn Sun, Haibin verfasserin aut Finite time integral sliding mode control of hypersonic vehicles 2013 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media Dordrecht 2013 Abstract This study investigates the tracking control problem for the longitudinal model of an airbreathing hypersonic vehicle (AHV) with external disturbances. By introducing finite time integral sliding mode manifolds, a novel finite time control method is designed for the longitudinal model of an AHV. This control method makes the velocity and altitude track the reference signals in finite time. Meanwhile, considering the large chattering phenomenon caused by high switching gains, an improved sliding mode control method based on nonlinear disturbance observer is proposed to reduce chattering. Through disturbance estimation for feedforward compensation, the improved sliding mode controller may take a smaller value for the switching gain without sacrificing disturbance rejection performance. Simulation results are provided to confirm the effectiveness of the proposed approach. Airbreathing hypersonic vehicle Sliding mode control Finite time stability Nonlinear disturbance observer Li, Shihua aut Sun, Changyin aut Enthalten in Nonlinear dynamics Springer Netherlands, 1990 73(2013), 1-2 vom: 30. Jan., Seite 229-244 (DE-627)130936782 (DE-600)1058624-6 (DE-576)034188126 0924-090X nnns volume:73 year:2013 number:1-2 day:30 month:01 pages:229-244 https://doi.org/10.1007/s11071-013-0780-4 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY SSG-OLC-CHE SSG-OLC-MAT SSG-OPC-MAT GBV_ILN_70 AR 73 2013 1-2 30 01 229-244 |
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10.1007/s11071-013-0780-4 doi (DE-627)OLC2051098115 (DE-He213)s11071-013-0780-4-p DE-627 ger DE-627 rakwb eng 510 VZ 11 ssgn Sun, Haibin verfasserin aut Finite time integral sliding mode control of hypersonic vehicles 2013 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media Dordrecht 2013 Abstract This study investigates the tracking control problem for the longitudinal model of an airbreathing hypersonic vehicle (AHV) with external disturbances. By introducing finite time integral sliding mode manifolds, a novel finite time control method is designed for the longitudinal model of an AHV. This control method makes the velocity and altitude track the reference signals in finite time. Meanwhile, considering the large chattering phenomenon caused by high switching gains, an improved sliding mode control method based on nonlinear disturbance observer is proposed to reduce chattering. Through disturbance estimation for feedforward compensation, the improved sliding mode controller may take a smaller value for the switching gain without sacrificing disturbance rejection performance. Simulation results are provided to confirm the effectiveness of the proposed approach. Airbreathing hypersonic vehicle Sliding mode control Finite time stability Nonlinear disturbance observer Li, Shihua aut Sun, Changyin aut Enthalten in Nonlinear dynamics Springer Netherlands, 1990 73(2013), 1-2 vom: 30. Jan., Seite 229-244 (DE-627)130936782 (DE-600)1058624-6 (DE-576)034188126 0924-090X nnns volume:73 year:2013 number:1-2 day:30 month:01 pages:229-244 https://doi.org/10.1007/s11071-013-0780-4 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY SSG-OLC-CHE SSG-OLC-MAT SSG-OPC-MAT GBV_ILN_70 AR 73 2013 1-2 30 01 229-244 |
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10.1007/s11071-013-0780-4 doi (DE-627)OLC2051098115 (DE-He213)s11071-013-0780-4-p DE-627 ger DE-627 rakwb eng 510 VZ 11 ssgn Sun, Haibin verfasserin aut Finite time integral sliding mode control of hypersonic vehicles 2013 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media Dordrecht 2013 Abstract This study investigates the tracking control problem for the longitudinal model of an airbreathing hypersonic vehicle (AHV) with external disturbances. By introducing finite time integral sliding mode manifolds, a novel finite time control method is designed for the longitudinal model of an AHV. This control method makes the velocity and altitude track the reference signals in finite time. Meanwhile, considering the large chattering phenomenon caused by high switching gains, an improved sliding mode control method based on nonlinear disturbance observer is proposed to reduce chattering. Through disturbance estimation for feedforward compensation, the improved sliding mode controller may take a smaller value for the switching gain without sacrificing disturbance rejection performance. Simulation results are provided to confirm the effectiveness of the proposed approach. Airbreathing hypersonic vehicle Sliding mode control Finite time stability Nonlinear disturbance observer Li, Shihua aut Sun, Changyin aut Enthalten in Nonlinear dynamics Springer Netherlands, 1990 73(2013), 1-2 vom: 30. Jan., Seite 229-244 (DE-627)130936782 (DE-600)1058624-6 (DE-576)034188126 0924-090X nnns volume:73 year:2013 number:1-2 day:30 month:01 pages:229-244 https://doi.org/10.1007/s11071-013-0780-4 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY SSG-OLC-CHE SSG-OLC-MAT SSG-OPC-MAT GBV_ILN_70 AR 73 2013 1-2 30 01 229-244 |
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Abstract This study investigates the tracking control problem for the longitudinal model of an airbreathing hypersonic vehicle (AHV) with external disturbances. By introducing finite time integral sliding mode manifolds, a novel finite time control method is designed for the longitudinal model of an AHV. This control method makes the velocity and altitude track the reference signals in finite time. Meanwhile, considering the large chattering phenomenon caused by high switching gains, an improved sliding mode control method based on nonlinear disturbance observer is proposed to reduce chattering. Through disturbance estimation for feedforward compensation, the improved sliding mode controller may take a smaller value for the switching gain without sacrificing disturbance rejection performance. Simulation results are provided to confirm the effectiveness of the proposed approach. © Springer Science+Business Media Dordrecht 2013 |
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Abstract This study investigates the tracking control problem for the longitudinal model of an airbreathing hypersonic vehicle (AHV) with external disturbances. By introducing finite time integral sliding mode manifolds, a novel finite time control method is designed for the longitudinal model of an AHV. This control method makes the velocity and altitude track the reference signals in finite time. Meanwhile, considering the large chattering phenomenon caused by high switching gains, an improved sliding mode control method based on nonlinear disturbance observer is proposed to reduce chattering. Through disturbance estimation for feedforward compensation, the improved sliding mode controller may take a smaller value for the switching gain without sacrificing disturbance rejection performance. Simulation results are provided to confirm the effectiveness of the proposed approach. © Springer Science+Business Media Dordrecht 2013 |
| abstract_unstemmed |
Abstract This study investigates the tracking control problem for the longitudinal model of an airbreathing hypersonic vehicle (AHV) with external disturbances. By introducing finite time integral sliding mode manifolds, a novel finite time control method is designed for the longitudinal model of an AHV. This control method makes the velocity and altitude track the reference signals in finite time. Meanwhile, considering the large chattering phenomenon caused by high switching gains, an improved sliding mode control method based on nonlinear disturbance observer is proposed to reduce chattering. Through disturbance estimation for feedforward compensation, the improved sliding mode controller may take a smaller value for the switching gain without sacrificing disturbance rejection performance. Simulation results are provided to confirm the effectiveness of the proposed approach. © Springer Science+Business Media Dordrecht 2013 |
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<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">OLC2051098115</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20230503225800.0</controlfield><controlfield tag="007">tu</controlfield><controlfield tag="008">200820s2013 xx ||||| 00| ||eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/s11071-013-0780-4</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)OLC2051098115</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-He213)s11071-013-0780-4-p</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">510</subfield><subfield code="q">VZ</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">11</subfield><subfield code="2">ssgn</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Sun, Haibin</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Finite time integral sliding mode control of hypersonic vehicles</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2013</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">ohne Hilfsmittel zu benutzen</subfield><subfield code="b">n</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Band</subfield><subfield code="b">nc</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© Springer Science+Business Media Dordrecht 2013</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract This study investigates the tracking control problem for the longitudinal model of an airbreathing hypersonic vehicle (AHV) with external disturbances. By introducing finite time integral sliding mode manifolds, a novel finite time control method is designed for the longitudinal model of an AHV. This control method makes the velocity and altitude track the reference signals in finite time. Meanwhile, considering the large chattering phenomenon caused by high switching gains, an improved sliding mode control method based on nonlinear disturbance observer is proposed to reduce chattering. Through disturbance estimation for feedforward compensation, the improved sliding mode controller may take a smaller value for the switching gain without sacrificing disturbance rejection performance. Simulation results are provided to confirm the effectiveness of the proposed approach.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Airbreathing hypersonic vehicle</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Sliding mode control</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Finite time stability</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Nonlinear disturbance observer</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Li, Shihua</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Sun, Changyin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">Nonlinear dynamics</subfield><subfield code="d">Springer Netherlands, 1990</subfield><subfield code="g">73(2013), 1-2 vom: 30. Jan., Seite 229-244</subfield><subfield code="w">(DE-627)130936782</subfield><subfield code="w">(DE-600)1058624-6</subfield><subfield code="w">(DE-576)034188126</subfield><subfield code="x">0924-090X</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:73</subfield><subfield code="g">year:2013</subfield><subfield code="g">number:1-2</subfield><subfield code="g">day:30</subfield><subfield code="g">month:01</subfield><subfield code="g">pages:229-244</subfield></datafield><datafield tag="856" ind1="4" ind2="1"><subfield code="u">https://doi.org/10.1007/s11071-013-0780-4</subfield><subfield code="z">lizenzpflichtig</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SYSFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_OLC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-TEC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-PHY</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-CHE</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-MAT</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OPC-MAT</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_70</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">73</subfield><subfield code="j">2013</subfield><subfield code="e">1-2</subfield><subfield code="b">30</subfield><subfield code="c">01</subfield><subfield code="h">229-244</subfield></datafield></record></collection>
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