Estimation of the determination accuracy of orbit parameters of the apophis asteroid from measurement results
Abstract An analysis of the existing astrometric and radar observations of the Apophis asteroid is performed. On the basis of this analysis, characteristics of future measurements of the asteroid orbit and limitation on their conduction are accepted. A proposed launching of a spacecraft to the aster...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Bakhshiyan, B. Ts. [verfasserIn] |
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| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2010 |
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| Schlagwörter: |
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| Anmerkung: |
© Pleiades Publishing, Ltd. 2010 |
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| Übergeordnetes Werk: |
Enthalten in: Cosmic research - SP MAIK Nauka/Interperiodica, 1964, 48(2010), 5 vom: Okt., Seite 417-423 |
|---|---|
| Übergeordnetes Werk: |
volume:48 ; year:2010 ; number:5 ; month:10 ; pages:417-423 |
| Links: |
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| DOI / URN: |
10.1134/S0010952510050072 |
|---|
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OLC2027384731 |
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| 520 | |a Abstract An analysis of the existing astrometric and radar observations of the Apophis asteroid is performed. On the basis of this analysis, characteristics of future measurements of the asteroid orbit and limitation on their conduction are accepted. A proposed launching of a spacecraft to the asteroid in order to obtain high-accuracy measurements of its distance and radial velocity is also considered. Trajectories of the flight to the asteroid in 2012–2022 are studied. Estimates of the accuracy of the Apophis position determination at various sets of both available and planned measurements at various numbers of determined parameters are obtained. The method of estimating accuracy is similar to that used in [1] for the Vega project. | ||
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10.1134/S0010952510050072 doi (DE-627)OLC2027384731 (DE-He213)S0010952510050072-p DE-627 ger DE-627 rakwb eng 520 620 VZ 16,12 ssgn Bakhshiyan, B. Ts. verfasserin aut Estimation of the determination accuracy of orbit parameters of the apophis asteroid from measurement results 2010 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Pleiades Publishing, Ltd. 2010 Abstract An analysis of the existing astrometric and radar observations of the Apophis asteroid is performed. On the basis of this analysis, characteristics of future measurements of the asteroid orbit and limitation on their conduction are accepted. A proposed launching of a spacecraft to the asteroid in order to obtain high-accuracy measurements of its distance and radial velocity is also considered. Trajectories of the flight to the asteroid in 2012–2022 are studied. Estimates of the accuracy of the Apophis position determination at various sets of both available and planned measurements at various numbers of determined parameters are obtained. The method of estimating accuracy is similar to that used in [1] for the Vega project. Radial Velocity Orbit Element Radio Telescope Cosmic Research Radar Measurement Sukhanov, A. A. aut Fedyaev, K. S. aut Enthalten in Cosmic research SP MAIK Nauka/Interperiodica, 1964 48(2010), 5 vom: Okt., Seite 417-423 (DE-627)129361909 (DE-600)160891-5 (DE-576)014734443 0010-9525 nnns volume:48 year:2010 number:5 month:10 pages:417-423 https://doi.org/10.1134/S0010952510050072 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-AST SSG-OPC-AST SSG-OPC-GEO SSG-OPC-GGO GBV_ILN_40 GBV_ILN_70 AR 48 2010 5 10 417-423 |
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10.1134/S0010952510050072 doi (DE-627)OLC2027384731 (DE-He213)S0010952510050072-p DE-627 ger DE-627 rakwb eng 520 620 VZ 16,12 ssgn Bakhshiyan, B. Ts. verfasserin aut Estimation of the determination accuracy of orbit parameters of the apophis asteroid from measurement results 2010 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Pleiades Publishing, Ltd. 2010 Abstract An analysis of the existing astrometric and radar observations of the Apophis asteroid is performed. On the basis of this analysis, characteristics of future measurements of the asteroid orbit and limitation on their conduction are accepted. A proposed launching of a spacecraft to the asteroid in order to obtain high-accuracy measurements of its distance and radial velocity is also considered. Trajectories of the flight to the asteroid in 2012–2022 are studied. Estimates of the accuracy of the Apophis position determination at various sets of both available and planned measurements at various numbers of determined parameters are obtained. The method of estimating accuracy is similar to that used in [1] for the Vega project. Radial Velocity Orbit Element Radio Telescope Cosmic Research Radar Measurement Sukhanov, A. A. aut Fedyaev, K. S. aut Enthalten in Cosmic research SP MAIK Nauka/Interperiodica, 1964 48(2010), 5 vom: Okt., Seite 417-423 (DE-627)129361909 (DE-600)160891-5 (DE-576)014734443 0010-9525 nnns volume:48 year:2010 number:5 month:10 pages:417-423 https://doi.org/10.1134/S0010952510050072 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-AST SSG-OPC-AST SSG-OPC-GEO SSG-OPC-GGO GBV_ILN_40 GBV_ILN_70 AR 48 2010 5 10 417-423 |
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10.1134/S0010952510050072 doi (DE-627)OLC2027384731 (DE-He213)S0010952510050072-p DE-627 ger DE-627 rakwb eng 520 620 VZ 16,12 ssgn Bakhshiyan, B. Ts. verfasserin aut Estimation of the determination accuracy of orbit parameters of the apophis asteroid from measurement results 2010 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Pleiades Publishing, Ltd. 2010 Abstract An analysis of the existing astrometric and radar observations of the Apophis asteroid is performed. On the basis of this analysis, characteristics of future measurements of the asteroid orbit and limitation on their conduction are accepted. A proposed launching of a spacecraft to the asteroid in order to obtain high-accuracy measurements of its distance and radial velocity is also considered. Trajectories of the flight to the asteroid in 2012–2022 are studied. Estimates of the accuracy of the Apophis position determination at various sets of both available and planned measurements at various numbers of determined parameters are obtained. The method of estimating accuracy is similar to that used in [1] for the Vega project. Radial Velocity Orbit Element Radio Telescope Cosmic Research Radar Measurement Sukhanov, A. A. aut Fedyaev, K. S. aut Enthalten in Cosmic research SP MAIK Nauka/Interperiodica, 1964 48(2010), 5 vom: Okt., Seite 417-423 (DE-627)129361909 (DE-600)160891-5 (DE-576)014734443 0010-9525 nnns volume:48 year:2010 number:5 month:10 pages:417-423 https://doi.org/10.1134/S0010952510050072 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-AST SSG-OPC-AST SSG-OPC-GEO SSG-OPC-GGO GBV_ILN_40 GBV_ILN_70 AR 48 2010 5 10 417-423 |
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estimation of the determination accuracy of orbit parameters of the apophis asteroid from measurement results |
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Estimation of the determination accuracy of orbit parameters of the apophis asteroid from measurement results |
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Abstract An analysis of the existing astrometric and radar observations of the Apophis asteroid is performed. On the basis of this analysis, characteristics of future measurements of the asteroid orbit and limitation on their conduction are accepted. A proposed launching of a spacecraft to the asteroid in order to obtain high-accuracy measurements of its distance and radial velocity is also considered. Trajectories of the flight to the asteroid in 2012–2022 are studied. Estimates of the accuracy of the Apophis position determination at various sets of both available and planned measurements at various numbers of determined parameters are obtained. The method of estimating accuracy is similar to that used in [1] for the Vega project. © Pleiades Publishing, Ltd. 2010 |
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Abstract An analysis of the existing astrometric and radar observations of the Apophis asteroid is performed. On the basis of this analysis, characteristics of future measurements of the asteroid orbit and limitation on their conduction are accepted. A proposed launching of a spacecraft to the asteroid in order to obtain high-accuracy measurements of its distance and radial velocity is also considered. Trajectories of the flight to the asteroid in 2012–2022 are studied. Estimates of the accuracy of the Apophis position determination at various sets of both available and planned measurements at various numbers of determined parameters are obtained. The method of estimating accuracy is similar to that used in [1] for the Vega project. © Pleiades Publishing, Ltd. 2010 |
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Abstract An analysis of the existing astrometric and radar observations of the Apophis asteroid is performed. On the basis of this analysis, characteristics of future measurements of the asteroid orbit and limitation on their conduction are accepted. A proposed launching of a spacecraft to the asteroid in order to obtain high-accuracy measurements of its distance and radial velocity is also considered. Trajectories of the flight to the asteroid in 2012–2022 are studied. Estimates of the accuracy of the Apophis position determination at various sets of both available and planned measurements at various numbers of determined parameters are obtained. The method of estimating accuracy is similar to that used in [1] for the Vega project. © Pleiades Publishing, Ltd. 2010 |
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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">OLC2027384731</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20230503033704.0</controlfield><controlfield tag="007">tu</controlfield><controlfield tag="008">200819s2010 xx ||||| 00| ||eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1134/S0010952510050072</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)OLC2027384731</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-He213)S0010952510050072-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">520</subfield><subfield code="a">620</subfield><subfield code="q">VZ</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">16,12</subfield><subfield code="2">ssgn</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Bakhshiyan, B. Ts.</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Estimation of the determination accuracy of orbit parameters of the apophis asteroid from measurement results</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2010</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">© Pleiades Publishing, Ltd. 2010</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract An analysis of the existing astrometric and radar observations of the Apophis asteroid is performed. On the basis of this analysis, characteristics of future measurements of the asteroid orbit and limitation on their conduction are accepted. A proposed launching of a spacecraft to the asteroid in order to obtain high-accuracy measurements of its distance and radial velocity is also considered. Trajectories of the flight to the asteroid in 2012–2022 are studied. Estimates of the accuracy of the Apophis position determination at various sets of both available and planned measurements at various numbers of determined parameters are obtained. 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S.</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">Cosmic research</subfield><subfield code="d">SP MAIK Nauka/Interperiodica, 1964</subfield><subfield code="g">48(2010), 5 vom: Okt., Seite 417-423</subfield><subfield code="w">(DE-627)129361909</subfield><subfield code="w">(DE-600)160891-5</subfield><subfield code="w">(DE-576)014734443</subfield><subfield code="x">0010-9525</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:48</subfield><subfield code="g">year:2010</subfield><subfield code="g">number:5</subfield><subfield code="g">month:10</subfield><subfield code="g">pages:417-423</subfield></datafield><datafield tag="856" ind1="4" ind2="1"><subfield code="u">https://doi.org/10.1134/S0010952510050072</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-AST</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OPC-AST</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OPC-GEO</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OPC-GGO</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_40</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">48</subfield><subfield code="j">2010</subfield><subfield code="e">5</subfield><subfield code="c">10</subfield><subfield code="h">417-423</subfield></datafield></record></collection>
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