Finite-time intercept-angle guidance
In this paper, new nonsingular terminal sliding mode control guidance laws (NTSMCGLs) to unknown maneuvering target intercept are proposed and their finite-time convergences are proved. A novel nonsingular terminal sliding mode surface based on a predefined angle is designed to improve intercept per...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Lu, Kunfeng [verfasserIn] |
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| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2015 |
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| Rechteinformationen: |
Nutzungsrecht: © 2014 Taylor & Francis 2014 |
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| Schlagwörter: |
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| Übergeordnetes Werk: |
Enthalten in: International journal of control - London : Taylor & Francis, 1965, 88(2015), 2, Seite 264-12 |
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| Übergeordnetes Werk: |
volume:88 ; year:2015 ; number:2 ; pages:264-12 |
| Links: |
|---|
| DOI / URN: |
10.1080/00207179.2014.949869 |
|---|
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OLC1962645495 |
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| 520 | |a In this paper, new nonsingular terminal sliding mode control guidance laws (NTSMCGLs) to unknown maneuvering target intercept are proposed and their finite-time convergences are proved. A novel nonsingular terminal sliding mode surface based on a predefined angle is designed to improve intercept performance and avoid singularity problem. The presented guidance law requires no information on maneuvering target that is estimated and compensated by extended state observer (ESO), and it can be used in practical systems where the target can evade freely. Also, undesired chattering is restrained effectively by real-time estimation and compensation of ESO. Simulation results show that the NTSMCGLs can achieve exact interception. | ||
| 540 | |a Nutzungsrecht: © 2014 Taylor & Francis 2014 | ||
| 650 | 4 | |a nonsingular terminal sliding mode control (NTSMC) | |
| 650 | 4 | |a extended state observer (ESO) | |
| 650 | 4 | |a finite-time control (FTC) | |
| 650 | 4 | |a intercept-angle constraint guidance (IACG) | |
| 700 | 1 | |a Xia, Yuanqing |4 oth | |
| 700 | 1 | |a Yu, Chunmei |4 oth | |
| 700 | 1 | |a Chen, Rongfang |4 oth | |
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10.1080/00207179.2014.949869 doi PQ20160617 (DE-627)OLC1962645495 (DE-599)GBVOLC1962645495 (PRQ)c2125-3a361184e00b8abafa37aa3d57310206bd68f2f750ef1513553d427adcbb08d40 (KEY)0006630320150000088000200264finitetimeinterceptangleguidance DE-627 ger DE-627 rakwb eng 620 DNB Lu, Kunfeng verfasserin aut Finite-time intercept-angle guidance 2015 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier In this paper, new nonsingular terminal sliding mode control guidance laws (NTSMCGLs) to unknown maneuvering target intercept are proposed and their finite-time convergences are proved. A novel nonsingular terminal sliding mode surface based on a predefined angle is designed to improve intercept performance and avoid singularity problem. The presented guidance law requires no information on maneuvering target that is estimated and compensated by extended state observer (ESO), and it can be used in practical systems where the target can evade freely. Also, undesired chattering is restrained effectively by real-time estimation and compensation of ESO. Simulation results show that the NTSMCGLs can achieve exact interception. Nutzungsrecht: © 2014 Taylor & Francis 2014 nonsingular terminal sliding mode control (NTSMC) extended state observer (ESO) finite-time control (FTC) intercept-angle constraint guidance (IACG) Xia, Yuanqing oth Yu, Chunmei oth Chen, Rongfang oth Enthalten in International journal of control London : Taylor & Francis, 1965 88(2015), 2, Seite 264-12 (DE-627)129595780 (DE-600)240693-7 (DE-576)015088804 0020-7179 nnns volume:88 year:2015 number:2 pages:264-12 http://dx.doi.org/10.1080/00207179.2014.949869 Volltext http://www.tandfonline.com/doi/abs/10.1080/00207179.2014.949869 http://search.proquest.com/docview/1640674708 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_21 GBV_ILN_70 GBV_ILN_2020 GBV_ILN_4314 GBV_ILN_4318 GBV_ILN_4700 AR 88 2015 2 264-12 |
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10.1080/00207179.2014.949869 doi PQ20160617 (DE-627)OLC1962645495 (DE-599)GBVOLC1962645495 (PRQ)c2125-3a361184e00b8abafa37aa3d57310206bd68f2f750ef1513553d427adcbb08d40 (KEY)0006630320150000088000200264finitetimeinterceptangleguidance DE-627 ger DE-627 rakwb eng 620 DNB Lu, Kunfeng verfasserin aut Finite-time intercept-angle guidance 2015 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier In this paper, new nonsingular terminal sliding mode control guidance laws (NTSMCGLs) to unknown maneuvering target intercept are proposed and their finite-time convergences are proved. A novel nonsingular terminal sliding mode surface based on a predefined angle is designed to improve intercept performance and avoid singularity problem. The presented guidance law requires no information on maneuvering target that is estimated and compensated by extended state observer (ESO), and it can be used in practical systems where the target can evade freely. Also, undesired chattering is restrained effectively by real-time estimation and compensation of ESO. Simulation results show that the NTSMCGLs can achieve exact interception. Nutzungsrecht: © 2014 Taylor & Francis 2014 nonsingular terminal sliding mode control (NTSMC) extended state observer (ESO) finite-time control (FTC) intercept-angle constraint guidance (IACG) Xia, Yuanqing oth Yu, Chunmei oth Chen, Rongfang oth Enthalten in International journal of control London : Taylor & Francis, 1965 88(2015), 2, Seite 264-12 (DE-627)129595780 (DE-600)240693-7 (DE-576)015088804 0020-7179 nnns volume:88 year:2015 number:2 pages:264-12 http://dx.doi.org/10.1080/00207179.2014.949869 Volltext http://www.tandfonline.com/doi/abs/10.1080/00207179.2014.949869 http://search.proquest.com/docview/1640674708 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_21 GBV_ILN_70 GBV_ILN_2020 GBV_ILN_4314 GBV_ILN_4318 GBV_ILN_4700 AR 88 2015 2 264-12 |
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10.1080/00207179.2014.949869 doi PQ20160617 (DE-627)OLC1962645495 (DE-599)GBVOLC1962645495 (PRQ)c2125-3a361184e00b8abafa37aa3d57310206bd68f2f750ef1513553d427adcbb08d40 (KEY)0006630320150000088000200264finitetimeinterceptangleguidance DE-627 ger DE-627 rakwb eng 620 DNB Lu, Kunfeng verfasserin aut Finite-time intercept-angle guidance 2015 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier In this paper, new nonsingular terminal sliding mode control guidance laws (NTSMCGLs) to unknown maneuvering target intercept are proposed and their finite-time convergences are proved. A novel nonsingular terminal sliding mode surface based on a predefined angle is designed to improve intercept performance and avoid singularity problem. The presented guidance law requires no information on maneuvering target that is estimated and compensated by extended state observer (ESO), and it can be used in practical systems where the target can evade freely. Also, undesired chattering is restrained effectively by real-time estimation and compensation of ESO. Simulation results show that the NTSMCGLs can achieve exact interception. Nutzungsrecht: © 2014 Taylor & Francis 2014 nonsingular terminal sliding mode control (NTSMC) extended state observer (ESO) finite-time control (FTC) intercept-angle constraint guidance (IACG) Xia, Yuanqing oth Yu, Chunmei oth Chen, Rongfang oth Enthalten in International journal of control London : Taylor & Francis, 1965 88(2015), 2, Seite 264-12 (DE-627)129595780 (DE-600)240693-7 (DE-576)015088804 0020-7179 nnns volume:88 year:2015 number:2 pages:264-12 http://dx.doi.org/10.1080/00207179.2014.949869 Volltext http://www.tandfonline.com/doi/abs/10.1080/00207179.2014.949869 http://search.proquest.com/docview/1640674708 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_21 GBV_ILN_70 GBV_ILN_2020 GBV_ILN_4314 GBV_ILN_4318 GBV_ILN_4700 AR 88 2015 2 264-12 |
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10.1080/00207179.2014.949869 doi PQ20160617 (DE-627)OLC1962645495 (DE-599)GBVOLC1962645495 (PRQ)c2125-3a361184e00b8abafa37aa3d57310206bd68f2f750ef1513553d427adcbb08d40 (KEY)0006630320150000088000200264finitetimeinterceptangleguidance DE-627 ger DE-627 rakwb eng 620 DNB Lu, Kunfeng verfasserin aut Finite-time intercept-angle guidance 2015 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier In this paper, new nonsingular terminal sliding mode control guidance laws (NTSMCGLs) to unknown maneuvering target intercept are proposed and their finite-time convergences are proved. A novel nonsingular terminal sliding mode surface based on a predefined angle is designed to improve intercept performance and avoid singularity problem. The presented guidance law requires no information on maneuvering target that is estimated and compensated by extended state observer (ESO), and it can be used in practical systems where the target can evade freely. Also, undesired chattering is restrained effectively by real-time estimation and compensation of ESO. Simulation results show that the NTSMCGLs can achieve exact interception. Nutzungsrecht: © 2014 Taylor & Francis 2014 nonsingular terminal sliding mode control (NTSMC) extended state observer (ESO) finite-time control (FTC) intercept-angle constraint guidance (IACG) Xia, Yuanqing oth Yu, Chunmei oth Chen, Rongfang oth Enthalten in International journal of control London : Taylor & Francis, 1965 88(2015), 2, Seite 264-12 (DE-627)129595780 (DE-600)240693-7 (DE-576)015088804 0020-7179 nnns volume:88 year:2015 number:2 pages:264-12 http://dx.doi.org/10.1080/00207179.2014.949869 Volltext http://www.tandfonline.com/doi/abs/10.1080/00207179.2014.949869 http://search.proquest.com/docview/1640674708 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_21 GBV_ILN_70 GBV_ILN_2020 GBV_ILN_4314 GBV_ILN_4318 GBV_ILN_4700 AR 88 2015 2 264-12 |
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10.1080/00207179.2014.949869 doi PQ20160617 (DE-627)OLC1962645495 (DE-599)GBVOLC1962645495 (PRQ)c2125-3a361184e00b8abafa37aa3d57310206bd68f2f750ef1513553d427adcbb08d40 (KEY)0006630320150000088000200264finitetimeinterceptangleguidance DE-627 ger DE-627 rakwb eng 620 DNB Lu, Kunfeng verfasserin aut Finite-time intercept-angle guidance 2015 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier In this paper, new nonsingular terminal sliding mode control guidance laws (NTSMCGLs) to unknown maneuvering target intercept are proposed and their finite-time convergences are proved. A novel nonsingular terminal sliding mode surface based on a predefined angle is designed to improve intercept performance and avoid singularity problem. The presented guidance law requires no information on maneuvering target that is estimated and compensated by extended state observer (ESO), and it can be used in practical systems where the target can evade freely. Also, undesired chattering is restrained effectively by real-time estimation and compensation of ESO. Simulation results show that the NTSMCGLs can achieve exact interception. Nutzungsrecht: © 2014 Taylor & Francis 2014 nonsingular terminal sliding mode control (NTSMC) extended state observer (ESO) finite-time control (FTC) intercept-angle constraint guidance (IACG) Xia, Yuanqing oth Yu, Chunmei oth Chen, Rongfang oth Enthalten in International journal of control London : Taylor & Francis, 1965 88(2015), 2, Seite 264-12 (DE-627)129595780 (DE-600)240693-7 (DE-576)015088804 0020-7179 nnns volume:88 year:2015 number:2 pages:264-12 http://dx.doi.org/10.1080/00207179.2014.949869 Volltext http://www.tandfonline.com/doi/abs/10.1080/00207179.2014.949869 http://search.proquest.com/docview/1640674708 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_21 GBV_ILN_70 GBV_ILN_2020 GBV_ILN_4314 GBV_ILN_4318 GBV_ILN_4700 AR 88 2015 2 264-12 |
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Lu, Kunfeng |
| doi_str_mv |
10.1080/00207179.2014.949869 |
| dewey-full |
620 |
| title_sort |
finite-time intercept-angle guidance |
| title_auth |
Finite-time intercept-angle guidance |
| abstract |
In this paper, new nonsingular terminal sliding mode control guidance laws (NTSMCGLs) to unknown maneuvering target intercept are proposed and their finite-time convergences are proved. A novel nonsingular terminal sliding mode surface based on a predefined angle is designed to improve intercept performance and avoid singularity problem. The presented guidance law requires no information on maneuvering target that is estimated and compensated by extended state observer (ESO), and it can be used in practical systems where the target can evade freely. Also, undesired chattering is restrained effectively by real-time estimation and compensation of ESO. Simulation results show that the NTSMCGLs can achieve exact interception. |
| abstractGer |
In this paper, new nonsingular terminal sliding mode control guidance laws (NTSMCGLs) to unknown maneuvering target intercept are proposed and their finite-time convergences are proved. A novel nonsingular terminal sliding mode surface based on a predefined angle is designed to improve intercept performance and avoid singularity problem. The presented guidance law requires no information on maneuvering target that is estimated and compensated by extended state observer (ESO), and it can be used in practical systems where the target can evade freely. Also, undesired chattering is restrained effectively by real-time estimation and compensation of ESO. Simulation results show that the NTSMCGLs can achieve exact interception. |
| abstract_unstemmed |
In this paper, new nonsingular terminal sliding mode control guidance laws (NTSMCGLs) to unknown maneuvering target intercept are proposed and their finite-time convergences are proved. A novel nonsingular terminal sliding mode surface based on a predefined angle is designed to improve intercept performance and avoid singularity problem. The presented guidance law requires no information on maneuvering target that is estimated and compensated by extended state observer (ESO), and it can be used in practical systems where the target can evade freely. Also, undesired chattering is restrained effectively by real-time estimation and compensation of ESO. Simulation results show that the NTSMCGLs can achieve exact interception. |
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| container_issue |
2 |
| title_short |
Finite-time intercept-angle guidance |
| url |
http://dx.doi.org/10.1080/00207179.2014.949869 http://www.tandfonline.com/doi/abs/10.1080/00207179.2014.949869 http://search.proquest.com/docview/1640674708 |
| remote_bool |
false |
| author2 |
Xia, Yuanqing Yu, Chunmei Chen, Rongfang |
| author2Str |
Xia, Yuanqing Yu, Chunmei Chen, Rongfang |
| ppnlink |
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| author2_role |
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| doi_str |
10.1080/00207179.2014.949869 |
| up_date |
2024-07-04T04:01:04.150Z |
| _version_ |
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7.40121 |