Adaptive control and orbit determination for elliptical rendezvous
In this paper, we study the control and orbit determination problems for elliptical rendezvous. Autonomous rendezvous is achieved by the proposed adaptive control based on the measurements of relative position and velocity between the chaser and target spacecraft. Moreover, the target orbital elemen...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Xu, Lijia [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2016 |
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| Schlagwörter: |
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| Umfang: |
6 |
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| Übergeordnetes Werk: |
Enthalten in: Sa1204 Does Intravenous Toradol Lower the Risk for Post- Endoscopic Retrograde Cholangiopancreatography Pancreatitis? - Al-Hamid, Hussein ELSEVIER, 2016, journal of the International Academy of Astronautics, Amsterdam [u.a.] |
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| Übergeordnetes Werk: |
volume:127 ; year:2016 ; pages:587-592 ; extent:6 |
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| DOI / URN: |
10.1016/j.actaastro.2016.06.035 |
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ELV029440580 |
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| 520 | |a In this paper, we study the control and orbit determination problems for elliptical rendezvous. Autonomous rendezvous is achieved by the proposed adaptive control based on the measurements of relative position and velocity between the chaser and target spacecraft. Moreover, the target orbital elements can be estimated during the rendezvous process. Finally, the effectiveness of the method is illustrated by simulations. | ||
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10.1016/j.actaastro.2016.06.035 doi GBVA2016002000003.pica (DE-627)ELV029440580 (ELSEVIER)S0094-5765(16)30584-7 DE-627 ger DE-627 rakwb eng 520 520 DE-600 610 VZ 600 670 VZ 51.00 bkl Xu, Lijia verfasserin aut Adaptive control and orbit determination for elliptical rendezvous 2016 6 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier In this paper, we study the control and orbit determination problems for elliptical rendezvous. Autonomous rendezvous is achieved by the proposed adaptive control based on the measurements of relative position and velocity between the chaser and target spacecraft. Moreover, the target orbital elements can be estimated during the rendezvous process. Finally, the effectiveness of the method is illustrated by simulations. Parameter estimation Elsevier Elliptical rendezvous Elsevier Orbit determination Elsevier Adaptive control Elsevier Hu, Yong oth Jiang, Tiantian oth Enthalten in Elsevier Science Al-Hamid, Hussein ELSEVIER Sa1204 Does Intravenous Toradol Lower the Risk for Post- Endoscopic Retrograde Cholangiopancreatography Pancreatitis? 2016 journal of the International Academy of Astronautics Amsterdam [u.a.] (DE-627)ELV014615371 volume:127 year:2016 pages:587-592 extent:6 https://doi.org/10.1016/j.actaastro.2016.06.035 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_40 GBV_ILN_105 GBV_ILN_2021 51.00 Werkstoffkunde: Allgemeines VZ AR 127 2016 587-592 6 045F 520 |
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10.1016/j.actaastro.2016.06.035 doi GBVA2016002000003.pica (DE-627)ELV029440580 (ELSEVIER)S0094-5765(16)30584-7 DE-627 ger DE-627 rakwb eng 520 520 DE-600 610 VZ 600 670 VZ 51.00 bkl Xu, Lijia verfasserin aut Adaptive control and orbit determination for elliptical rendezvous 2016 6 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier In this paper, we study the control and orbit determination problems for elliptical rendezvous. Autonomous rendezvous is achieved by the proposed adaptive control based on the measurements of relative position and velocity between the chaser and target spacecraft. Moreover, the target orbital elements can be estimated during the rendezvous process. Finally, the effectiveness of the method is illustrated by simulations. Parameter estimation Elsevier Elliptical rendezvous Elsevier Orbit determination Elsevier Adaptive control Elsevier Hu, Yong oth Jiang, Tiantian oth Enthalten in Elsevier Science Al-Hamid, Hussein ELSEVIER Sa1204 Does Intravenous Toradol Lower the Risk for Post- Endoscopic Retrograde Cholangiopancreatography Pancreatitis? 2016 journal of the International Academy of Astronautics Amsterdam [u.a.] (DE-627)ELV014615371 volume:127 year:2016 pages:587-592 extent:6 https://doi.org/10.1016/j.actaastro.2016.06.035 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_40 GBV_ILN_105 GBV_ILN_2021 51.00 Werkstoffkunde: Allgemeines VZ AR 127 2016 587-592 6 045F 520 |
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10.1016/j.actaastro.2016.06.035 doi GBVA2016002000003.pica (DE-627)ELV029440580 (ELSEVIER)S0094-5765(16)30584-7 DE-627 ger DE-627 rakwb eng 520 520 DE-600 610 VZ 600 670 VZ 51.00 bkl Xu, Lijia verfasserin aut Adaptive control and orbit determination for elliptical rendezvous 2016 6 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier In this paper, we study the control and orbit determination problems for elliptical rendezvous. Autonomous rendezvous is achieved by the proposed adaptive control based on the measurements of relative position and velocity between the chaser and target spacecraft. Moreover, the target orbital elements can be estimated during the rendezvous process. Finally, the effectiveness of the method is illustrated by simulations. Parameter estimation Elsevier Elliptical rendezvous Elsevier Orbit determination Elsevier Adaptive control Elsevier Hu, Yong oth Jiang, Tiantian oth Enthalten in Elsevier Science Al-Hamid, Hussein ELSEVIER Sa1204 Does Intravenous Toradol Lower the Risk for Post- Endoscopic Retrograde Cholangiopancreatography Pancreatitis? 2016 journal of the International Academy of Astronautics Amsterdam [u.a.] (DE-627)ELV014615371 volume:127 year:2016 pages:587-592 extent:6 https://doi.org/10.1016/j.actaastro.2016.06.035 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_40 GBV_ILN_105 GBV_ILN_2021 51.00 Werkstoffkunde: Allgemeines VZ AR 127 2016 587-592 6 045F 520 |
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10.1016/j.actaastro.2016.06.035 doi GBVA2016002000003.pica (DE-627)ELV029440580 (ELSEVIER)S0094-5765(16)30584-7 DE-627 ger DE-627 rakwb eng 520 520 DE-600 610 VZ 600 670 VZ 51.00 bkl Xu, Lijia verfasserin aut Adaptive control and orbit determination for elliptical rendezvous 2016 6 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier In this paper, we study the control and orbit determination problems for elliptical rendezvous. Autonomous rendezvous is achieved by the proposed adaptive control based on the measurements of relative position and velocity between the chaser and target spacecraft. Moreover, the target orbital elements can be estimated during the rendezvous process. Finally, the effectiveness of the method is illustrated by simulations. Parameter estimation Elsevier Elliptical rendezvous Elsevier Orbit determination Elsevier Adaptive control Elsevier Hu, Yong oth Jiang, Tiantian oth Enthalten in Elsevier Science Al-Hamid, Hussein ELSEVIER Sa1204 Does Intravenous Toradol Lower the Risk for Post- Endoscopic Retrograde Cholangiopancreatography Pancreatitis? 2016 journal of the International Academy of Astronautics Amsterdam [u.a.] (DE-627)ELV014615371 volume:127 year:2016 pages:587-592 extent:6 https://doi.org/10.1016/j.actaastro.2016.06.035 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_40 GBV_ILN_105 GBV_ILN_2021 51.00 Werkstoffkunde: Allgemeines VZ AR 127 2016 587-592 6 045F 520 |
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In this paper, we study the control and orbit determination problems for elliptical rendezvous. Autonomous rendezvous is achieved by the proposed adaptive control based on the measurements of relative position and velocity between the chaser and target spacecraft. Moreover, the target orbital elements can be estimated during the rendezvous process. Finally, the effectiveness of the method is illustrated by simulations. |
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In this paper, we study the control and orbit determination problems for elliptical rendezvous. Autonomous rendezvous is achieved by the proposed adaptive control based on the measurements of relative position and velocity between the chaser and target spacecraft. Moreover, the target orbital elements can be estimated during the rendezvous process. Finally, the effectiveness of the method is illustrated by simulations. |
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In this paper, we study the control and orbit determination problems for elliptical rendezvous. Autonomous rendezvous is achieved by the proposed adaptive control based on the measurements of relative position and velocity between the chaser and target spacecraft. Moreover, the target orbital elements can be estimated during the rendezvous process. Finally, the effectiveness of the method is illustrated by simulations. |
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