Optimal feedback control of the deployment of a tethered subsatellite subject to perturbations
Abstract This paper presents the nonlinear optimal feedback control for the deployment process of a tethered subsatellite model, which involves not only the usually addressed in-plane motion, but also the out-of-plane motion. The model also takes the uncertainties in the mass parameter, the perturba...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Wen, H. [verfasserIn] |
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| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2007 |
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| Schlagwörter: |
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| Anmerkung: |
© Springer Science+Business Media, Inc. 2007 |
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| Übergeordnetes Werk: |
Enthalten in: Nonlinear dynamics - Springer Netherlands, 1990, 51(2007), 4 vom: 28. Feb., Seite 501-514 |
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| Übergeordnetes Werk: |
volume:51 ; year:2007 ; number:4 ; day:28 ; month:02 ; pages:501-514 |
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| DOI / URN: |
10.1007/s11071-007-9240-3 |
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| 520 | |a Abstract This paper presents the nonlinear optimal feedback control for the deployment process of a tethered subsatellite model, which involves not only the usually addressed in-plane motion, but also the out-of-plane motion. The model also takes the uncertainties in the mass parameter, the perturbations in initial states, and the external disturbance forces into consideration from an engineering point of view. The proposed controller is on the basis of a shrinking horizon and online grid adaptation scheme. Even though the proposed feedback law is not analytically explicit, it is easy to determine it by using a rapid recomputation of the open-loop optimal control, which generates the initial guesses for controls by interpolating the results from the previous computation. The case studies in the paper well demonstrate the effectiveness, robustness, and dominant real-time merits of the proposed controller. | ||
| 650 | 4 | |a Tethered subsatellite system | |
| 650 | 4 | |a Optimal feedback control | |
| 650 | 4 | |a Out-of-plane motion | |
| 700 | 1 | |a Jin, D. P. |4 aut | |
| 700 | 1 | |a Hu, H. Y. |4 aut | |
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10.1007/s11071-007-9240-3 doi (DE-627)OLC2051083525 (DE-He213)s11071-007-9240-3-p DE-627 ger DE-627 rakwb eng 510 VZ 11 ssgn Wen, H. verfasserin aut Optimal feedback control of the deployment of a tethered subsatellite subject to perturbations 2007 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media, Inc. 2007 Abstract This paper presents the nonlinear optimal feedback control for the deployment process of a tethered subsatellite model, which involves not only the usually addressed in-plane motion, but also the out-of-plane motion. The model also takes the uncertainties in the mass parameter, the perturbations in initial states, and the external disturbance forces into consideration from an engineering point of view. The proposed controller is on the basis of a shrinking horizon and online grid adaptation scheme. Even though the proposed feedback law is not analytically explicit, it is easy to determine it by using a rapid recomputation of the open-loop optimal control, which generates the initial guesses for controls by interpolating the results from the previous computation. The case studies in the paper well demonstrate the effectiveness, robustness, and dominant real-time merits of the proposed controller. Tethered subsatellite system Optimal feedback control Out-of-plane motion Jin, D. P. aut Hu, H. Y. aut Enthalten in Nonlinear dynamics Springer Netherlands, 1990 51(2007), 4 vom: 28. Feb., Seite 501-514 (DE-627)130936782 (DE-600)1058624-6 (DE-576)034188126 0924-090X nnns volume:51 year:2007 number:4 day:28 month:02 pages:501-514 https://doi.org/10.1007/s11071-007-9240-3 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_23 GBV_ILN_70 GBV_ILN_2006 GBV_ILN_4307 AR 51 2007 4 28 02 501-514 |
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10.1007/s11071-007-9240-3 doi (DE-627)OLC2051083525 (DE-He213)s11071-007-9240-3-p DE-627 ger DE-627 rakwb eng 510 VZ 11 ssgn Wen, H. verfasserin aut Optimal feedback control of the deployment of a tethered subsatellite subject to perturbations 2007 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media, Inc. 2007 Abstract This paper presents the nonlinear optimal feedback control for the deployment process of a tethered subsatellite model, which involves not only the usually addressed in-plane motion, but also the out-of-plane motion. The model also takes the uncertainties in the mass parameter, the perturbations in initial states, and the external disturbance forces into consideration from an engineering point of view. The proposed controller is on the basis of a shrinking horizon and online grid adaptation scheme. Even though the proposed feedback law is not analytically explicit, it is easy to determine it by using a rapid recomputation of the open-loop optimal control, which generates the initial guesses for controls by interpolating the results from the previous computation. The case studies in the paper well demonstrate the effectiveness, robustness, and dominant real-time merits of the proposed controller. Tethered subsatellite system Optimal feedback control Out-of-plane motion Jin, D. P. aut Hu, H. Y. aut Enthalten in Nonlinear dynamics Springer Netherlands, 1990 51(2007), 4 vom: 28. Feb., Seite 501-514 (DE-627)130936782 (DE-600)1058624-6 (DE-576)034188126 0924-090X nnns volume:51 year:2007 number:4 day:28 month:02 pages:501-514 https://doi.org/10.1007/s11071-007-9240-3 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_23 GBV_ILN_70 GBV_ILN_2006 GBV_ILN_4307 AR 51 2007 4 28 02 501-514 |
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10.1007/s11071-007-9240-3 doi (DE-627)OLC2051083525 (DE-He213)s11071-007-9240-3-p DE-627 ger DE-627 rakwb eng 510 VZ 11 ssgn Wen, H. verfasserin aut Optimal feedback control of the deployment of a tethered subsatellite subject to perturbations 2007 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media, Inc. 2007 Abstract This paper presents the nonlinear optimal feedback control for the deployment process of a tethered subsatellite model, which involves not only the usually addressed in-plane motion, but also the out-of-plane motion. The model also takes the uncertainties in the mass parameter, the perturbations in initial states, and the external disturbance forces into consideration from an engineering point of view. The proposed controller is on the basis of a shrinking horizon and online grid adaptation scheme. Even though the proposed feedback law is not analytically explicit, it is easy to determine it by using a rapid recomputation of the open-loop optimal control, which generates the initial guesses for controls by interpolating the results from the previous computation. The case studies in the paper well demonstrate the effectiveness, robustness, and dominant real-time merits of the proposed controller. Tethered subsatellite system Optimal feedback control Out-of-plane motion Jin, D. P. aut Hu, H. Y. aut Enthalten in Nonlinear dynamics Springer Netherlands, 1990 51(2007), 4 vom: 28. Feb., Seite 501-514 (DE-627)130936782 (DE-600)1058624-6 (DE-576)034188126 0924-090X nnns volume:51 year:2007 number:4 day:28 month:02 pages:501-514 https://doi.org/10.1007/s11071-007-9240-3 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_23 GBV_ILN_70 GBV_ILN_2006 GBV_ILN_4307 AR 51 2007 4 28 02 501-514 |
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10.1007/s11071-007-9240-3 doi (DE-627)OLC2051083525 (DE-He213)s11071-007-9240-3-p DE-627 ger DE-627 rakwb eng 510 VZ 11 ssgn Wen, H. verfasserin aut Optimal feedback control of the deployment of a tethered subsatellite subject to perturbations 2007 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media, Inc. 2007 Abstract This paper presents the nonlinear optimal feedback control for the deployment process of a tethered subsatellite model, which involves not only the usually addressed in-plane motion, but also the out-of-plane motion. The model also takes the uncertainties in the mass parameter, the perturbations in initial states, and the external disturbance forces into consideration from an engineering point of view. The proposed controller is on the basis of a shrinking horizon and online grid adaptation scheme. Even though the proposed feedback law is not analytically explicit, it is easy to determine it by using a rapid recomputation of the open-loop optimal control, which generates the initial guesses for controls by interpolating the results from the previous computation. The case studies in the paper well demonstrate the effectiveness, robustness, and dominant real-time merits of the proposed controller. Tethered subsatellite system Optimal feedback control Out-of-plane motion Jin, D. P. aut Hu, H. Y. aut Enthalten in Nonlinear dynamics Springer Netherlands, 1990 51(2007), 4 vom: 28. Feb., Seite 501-514 (DE-627)130936782 (DE-600)1058624-6 (DE-576)034188126 0924-090X nnns volume:51 year:2007 number:4 day:28 month:02 pages:501-514 https://doi.org/10.1007/s11071-007-9240-3 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_23 GBV_ILN_70 GBV_ILN_2006 GBV_ILN_4307 AR 51 2007 4 28 02 501-514 |
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10.1007/s11071-007-9240-3 doi (DE-627)OLC2051083525 (DE-He213)s11071-007-9240-3-p DE-627 ger DE-627 rakwb eng 510 VZ 11 ssgn Wen, H. verfasserin aut Optimal feedback control of the deployment of a tethered subsatellite subject to perturbations 2007 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media, Inc. 2007 Abstract This paper presents the nonlinear optimal feedback control for the deployment process of a tethered subsatellite model, which involves not only the usually addressed in-plane motion, but also the out-of-plane motion. The model also takes the uncertainties in the mass parameter, the perturbations in initial states, and the external disturbance forces into consideration from an engineering point of view. The proposed controller is on the basis of a shrinking horizon and online grid adaptation scheme. Even though the proposed feedback law is not analytically explicit, it is easy to determine it by using a rapid recomputation of the open-loop optimal control, which generates the initial guesses for controls by interpolating the results from the previous computation. The case studies in the paper well demonstrate the effectiveness, robustness, and dominant real-time merits of the proposed controller. Tethered subsatellite system Optimal feedback control Out-of-plane motion Jin, D. P. aut Hu, H. Y. aut Enthalten in Nonlinear dynamics Springer Netherlands, 1990 51(2007), 4 vom: 28. Feb., Seite 501-514 (DE-627)130936782 (DE-600)1058624-6 (DE-576)034188126 0924-090X nnns volume:51 year:2007 number:4 day:28 month:02 pages:501-514 https://doi.org/10.1007/s11071-007-9240-3 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_23 GBV_ILN_70 GBV_ILN_2006 GBV_ILN_4307 AR 51 2007 4 28 02 501-514 |
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Optimal feedback control of the deployment of a tethered subsatellite subject to perturbations |
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Abstract This paper presents the nonlinear optimal feedback control for the deployment process of a tethered subsatellite model, which involves not only the usually addressed in-plane motion, but also the out-of-plane motion. The model also takes the uncertainties in the mass parameter, the perturbations in initial states, and the external disturbance forces into consideration from an engineering point of view. The proposed controller is on the basis of a shrinking horizon and online grid adaptation scheme. Even though the proposed feedback law is not analytically explicit, it is easy to determine it by using a rapid recomputation of the open-loop optimal control, which generates the initial guesses for controls by interpolating the results from the previous computation. The case studies in the paper well demonstrate the effectiveness, robustness, and dominant real-time merits of the proposed controller. © Springer Science+Business Media, Inc. 2007 |
| abstractGer |
Abstract This paper presents the nonlinear optimal feedback control for the deployment process of a tethered subsatellite model, which involves not only the usually addressed in-plane motion, but also the out-of-plane motion. The model also takes the uncertainties in the mass parameter, the perturbations in initial states, and the external disturbance forces into consideration from an engineering point of view. The proposed controller is on the basis of a shrinking horizon and online grid adaptation scheme. Even though the proposed feedback law is not analytically explicit, it is easy to determine it by using a rapid recomputation of the open-loop optimal control, which generates the initial guesses for controls by interpolating the results from the previous computation. The case studies in the paper well demonstrate the effectiveness, robustness, and dominant real-time merits of the proposed controller. © Springer Science+Business Media, Inc. 2007 |
| abstract_unstemmed |
Abstract This paper presents the nonlinear optimal feedback control for the deployment process of a tethered subsatellite model, which involves not only the usually addressed in-plane motion, but also the out-of-plane motion. The model also takes the uncertainties in the mass parameter, the perturbations in initial states, and the external disturbance forces into consideration from an engineering point of view. The proposed controller is on the basis of a shrinking horizon and online grid adaptation scheme. Even though the proposed feedback law is not analytically explicit, it is easy to determine it by using a rapid recomputation of the open-loop optimal control, which generates the initial guesses for controls by interpolating the results from the previous computation. The case studies in the paper well demonstrate the effectiveness, robustness, and dominant real-time merits of the proposed controller. © Springer Science+Business Media, Inc. 2007 |
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Optimal feedback control of the deployment of a tethered subsatellite subject to perturbations |
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https://doi.org/10.1007/s11071-007-9240-3 |
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Jin, D. P. Hu, H. Y. |
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10.1007/s11071-007-9240-3 |
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