Deployment of Reconfigurable Spacecraft Under Earth Conditions in the Out-Of-Plane Rotation Mode
Abstract The cable-suspension method is used to simulate weightlessness on Earth in the general case. By an example of mathematical simulation of a system of rigid bodies connected via hinged joints and suspended from a special facility, it is shown that the method developed provides realistic simul...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Alpatov, A. P. [verfasserIn] |
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| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2000 |
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| Schlagwörter: |
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| Anmerkung: |
© Plenum Publishing Corporation 2000 |
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| Übergeordnetes Werk: |
Enthalten in: International applied mechanics - Kluwer Academic Publishers-Plenum Publishers, 1993, 36(2000), 10 vom: Okt., Seite 1385-1392 |
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| Übergeordnetes Werk: |
volume:36 ; year:2000 ; number:10 ; month:10 ; pages:1385-1392 |
| Links: |
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| DOI / URN: |
10.1023/A:1009450620060 |
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OLC2075719810 |
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| 520 | |a Abstract The cable-suspension method is used to simulate weightlessness on Earth in the general case. By an example of mathematical simulation of a system of rigid bodies connected via hinged joints and suspended from a special facility, it is shown that the method developed provides realistic simulation of orbital processes under earth conditions. The validation criterion for the simulation is the closeness of the values of the forces and moments in joints and the attitude and angular velocities to their theoretical values in orbital motion | ||
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| 700 | 1 | |a Khoroshilov, V. S. |4 aut | |
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10.1023/A:1009450620060 doi (DE-627)OLC2075719810 (DE-He213)A:1009450620060-p DE-627 ger DE-627 rakwb eng 530 VZ Alpatov, A. P. verfasserin aut Deployment of Reconfigurable Spacecraft Under Earth Conditions in the Out-Of-Plane Rotation Mode 2000 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Plenum Publishing Corporation 2000 Abstract The cable-suspension method is used to simulate weightlessness on Earth in the general case. By an example of mathematical simulation of a system of rigid bodies connected via hinged joints and suspended from a special facility, it is shown that the method developed provides realistic simulation of orbital processes under earth conditions. The validation criterion for the simulation is the closeness of the values of the forces and moments in joints and the attitude and angular velocities to their theoretical values in orbital motion Angular Velocity Rigid Body Validation Criterion Mathematical Simulation Realistic Simulation Dranovskii, V. I. aut Zakrzhevskii, A. E. aut Saltykov, Yu. D. aut Khoroshilov, V. S. aut Enthalten in International applied mechanics Kluwer Academic Publishers-Plenum Publishers, 1993 36(2000), 10 vom: Okt., Seite 1385-1392 (DE-627)131145630 (DE-600)1128258-7 (DE-576)032855141 1063-7095 nnns volume:36 year:2000 number:10 month:10 pages:1385-1392 https://doi.org/10.1023/A:1009450620060 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_32 GBV_ILN_70 AR 36 2000 10 10 1385-1392 |
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10.1023/A:1009450620060 doi (DE-627)OLC2075719810 (DE-He213)A:1009450620060-p DE-627 ger DE-627 rakwb eng 530 VZ Alpatov, A. P. verfasserin aut Deployment of Reconfigurable Spacecraft Under Earth Conditions in the Out-Of-Plane Rotation Mode 2000 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Plenum Publishing Corporation 2000 Abstract The cable-suspension method is used to simulate weightlessness on Earth in the general case. By an example of mathematical simulation of a system of rigid bodies connected via hinged joints and suspended from a special facility, it is shown that the method developed provides realistic simulation of orbital processes under earth conditions. The validation criterion for the simulation is the closeness of the values of the forces and moments in joints and the attitude and angular velocities to their theoretical values in orbital motion Angular Velocity Rigid Body Validation Criterion Mathematical Simulation Realistic Simulation Dranovskii, V. I. aut Zakrzhevskii, A. E. aut Saltykov, Yu. D. aut Khoroshilov, V. S. aut Enthalten in International applied mechanics Kluwer Academic Publishers-Plenum Publishers, 1993 36(2000), 10 vom: Okt., Seite 1385-1392 (DE-627)131145630 (DE-600)1128258-7 (DE-576)032855141 1063-7095 nnns volume:36 year:2000 number:10 month:10 pages:1385-1392 https://doi.org/10.1023/A:1009450620060 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_32 GBV_ILN_70 AR 36 2000 10 10 1385-1392 |
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10.1023/A:1009450620060 doi (DE-627)OLC2075719810 (DE-He213)A:1009450620060-p DE-627 ger DE-627 rakwb eng 530 VZ Alpatov, A. P. verfasserin aut Deployment of Reconfigurable Spacecraft Under Earth Conditions in the Out-Of-Plane Rotation Mode 2000 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Plenum Publishing Corporation 2000 Abstract The cable-suspension method is used to simulate weightlessness on Earth in the general case. By an example of mathematical simulation of a system of rigid bodies connected via hinged joints and suspended from a special facility, it is shown that the method developed provides realistic simulation of orbital processes under earth conditions. The validation criterion for the simulation is the closeness of the values of the forces and moments in joints and the attitude and angular velocities to their theoretical values in orbital motion Angular Velocity Rigid Body Validation Criterion Mathematical Simulation Realistic Simulation Dranovskii, V. I. aut Zakrzhevskii, A. E. aut Saltykov, Yu. D. aut Khoroshilov, V. S. aut Enthalten in International applied mechanics Kluwer Academic Publishers-Plenum Publishers, 1993 36(2000), 10 vom: Okt., Seite 1385-1392 (DE-627)131145630 (DE-600)1128258-7 (DE-576)032855141 1063-7095 nnns volume:36 year:2000 number:10 month:10 pages:1385-1392 https://doi.org/10.1023/A:1009450620060 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_32 GBV_ILN_70 AR 36 2000 10 10 1385-1392 |
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10.1023/A:1009450620060 doi (DE-627)OLC2075719810 (DE-He213)A:1009450620060-p DE-627 ger DE-627 rakwb eng 530 VZ Alpatov, A. P. verfasserin aut Deployment of Reconfigurable Spacecraft Under Earth Conditions in the Out-Of-Plane Rotation Mode 2000 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Plenum Publishing Corporation 2000 Abstract The cable-suspension method is used to simulate weightlessness on Earth in the general case. By an example of mathematical simulation of a system of rigid bodies connected via hinged joints and suspended from a special facility, it is shown that the method developed provides realistic simulation of orbital processes under earth conditions. The validation criterion for the simulation is the closeness of the values of the forces and moments in joints and the attitude and angular velocities to their theoretical values in orbital motion Angular Velocity Rigid Body Validation Criterion Mathematical Simulation Realistic Simulation Dranovskii, V. I. aut Zakrzhevskii, A. E. aut Saltykov, Yu. D. aut Khoroshilov, V. S. aut Enthalten in International applied mechanics Kluwer Academic Publishers-Plenum Publishers, 1993 36(2000), 10 vom: Okt., Seite 1385-1392 (DE-627)131145630 (DE-600)1128258-7 (DE-576)032855141 1063-7095 nnns volume:36 year:2000 number:10 month:10 pages:1385-1392 https://doi.org/10.1023/A:1009450620060 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_32 GBV_ILN_70 AR 36 2000 10 10 1385-1392 |
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Abstract The cable-suspension method is used to simulate weightlessness on Earth in the general case. By an example of mathematical simulation of a system of rigid bodies connected via hinged joints and suspended from a special facility, it is shown that the method developed provides realistic simulation of orbital processes under earth conditions. The validation criterion for the simulation is the closeness of the values of the forces and moments in joints and the attitude and angular velocities to their theoretical values in orbital motion © Plenum Publishing Corporation 2000 |
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Abstract The cable-suspension method is used to simulate weightlessness on Earth in the general case. By an example of mathematical simulation of a system of rigid bodies connected via hinged joints and suspended from a special facility, it is shown that the method developed provides realistic simulation of orbital processes under earth conditions. The validation criterion for the simulation is the closeness of the values of the forces and moments in joints and the attitude and angular velocities to their theoretical values in orbital motion © Plenum Publishing Corporation 2000 |
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Abstract The cable-suspension method is used to simulate weightlessness on Earth in the general case. By an example of mathematical simulation of a system of rigid bodies connected via hinged joints and suspended from a special facility, it is shown that the method developed provides realistic simulation of orbital processes under earth conditions. The validation criterion for the simulation is the closeness of the values of the forces and moments in joints and the attitude and angular velocities to their theoretical values in orbital motion © Plenum Publishing Corporation 2000 |
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P.</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Deployment of Reconfigurable Spacecraft Under Earth Conditions in the Out-Of-Plane Rotation Mode</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2000</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">© Plenum Publishing Corporation 2000</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract The cable-suspension method is used to simulate weightlessness on Earth in the general case. By an example of mathematical simulation of a system of rigid bodies connected via hinged joints and suspended from a special facility, it is shown that the method developed provides realistic simulation of orbital processes under earth conditions. The validation criterion for the simulation is the closeness of the values of the forces and moments in joints and the attitude and angular velocities to their theoretical values in orbital motion</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Angular Velocity</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Rigid Body</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Validation Criterion</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Mathematical Simulation</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Realistic Simulation</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Dranovskii, V. I.</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Zakrzhevskii, A. 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