On one technique for determining the spacecraft attitude prom the sun
Abstract A variant to implement a spacecraft (SC) spatial attitude system with respect to the Sun is discussed. The sunward direction and the solar rotation axis are used as reference points. The system is based on measuring spectral line Doppler shift by scanning the solar image along the limb and...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
1994 |
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| Umfang: |
13 |
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| Reproduktion: |
Springer Online Journal Archives 1860-2002 |
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| Übergeordnetes Werk: |
in: Experimental astronomy - 1989, 5(1994) vom: März/Apr., Seite 301-313 |
| Übergeordnetes Werk: |
volume:5 ; year:1994 ; month:03/04 ; pages:301-313 ; extent:13 |
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NLEJ193934531 |
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| 520 | |a Abstract A variant to implement a spacecraft (SC) spatial attitude system with respect to the Sun is discussed. The sunward direction and the solar rotation axis are used as reference points. The system is based on measuring spectral line Doppler shift by scanning the solar image along the limb and is self-adjusting for relative spectral line shifts and instrument band shifts. The first harmonic of the signal serves as a basis for accurate adjustment of filter band. The second harmonic phase is used to measure the spacecraft attitude. The application of this method holds the greatest promise when the SO is stabilized by the sunward spinning because this ensures continuous monitoring of the spacecraft attitude.In addition, the method provides information on the precise coordinates of solar surface details during space-borne observations. | ||
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(DE-627)NLEJ193934531 DE-627 ger DE-627 rakwb eng On one technique for determining the spacecraft attitude prom the sun 1994 13 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Abstract A variant to implement a spacecraft (SC) spatial attitude system with respect to the Sun is discussed. The sunward direction and the solar rotation axis are used as reference points. The system is based on measuring spectral line Doppler shift by scanning the solar image along the limb and is self-adjusting for relative spectral line shifts and instrument band shifts. The first harmonic of the signal serves as a basis for accurate adjustment of filter band. The second harmonic phase is used to measure the spacecraft attitude. The application of this method holds the greatest promise when the SO is stabilized by the sunward spinning because this ensures continuous monitoring of the spacecraft attitude.In addition, the method provides information on the precise coordinates of solar surface details during space-borne observations. Springer Online Journal Archives 1860-2002 Kobanov, N. I. oth in Experimental astronomy 1989 5(1994) vom: März/Apr., Seite 301-313 (DE-627)NLEJ188994203 (DE-600)2012330-9 1572-9508 nnns volume:5 year:1994 month:03/04 pages:301-313 extent:13 http://dx.doi.org/10.1007/BF01583703 GBV_USEFLAG_U ZDB-1-SOJ GBV_NL_ARTICLE AR 5 1994 3/4 301-313 13 |
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(DE-627)NLEJ193934531 DE-627 ger DE-627 rakwb eng On one technique for determining the spacecraft attitude prom the sun 1994 13 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Abstract A variant to implement a spacecraft (SC) spatial attitude system with respect to the Sun is discussed. The sunward direction and the solar rotation axis are used as reference points. The system is based on measuring spectral line Doppler shift by scanning the solar image along the limb and is self-adjusting for relative spectral line shifts and instrument band shifts. The first harmonic of the signal serves as a basis for accurate adjustment of filter band. The second harmonic phase is used to measure the spacecraft attitude. The application of this method holds the greatest promise when the SO is stabilized by the sunward spinning because this ensures continuous monitoring of the spacecraft attitude.In addition, the method provides information on the precise coordinates of solar surface details during space-borne observations. Springer Online Journal Archives 1860-2002 Kobanov, N. I. oth in Experimental astronomy 1989 5(1994) vom: März/Apr., Seite 301-313 (DE-627)NLEJ188994203 (DE-600)2012330-9 1572-9508 nnns volume:5 year:1994 month:03/04 pages:301-313 extent:13 http://dx.doi.org/10.1007/BF01583703 GBV_USEFLAG_U ZDB-1-SOJ GBV_NL_ARTICLE AR 5 1994 3/4 301-313 13 |
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(DE-627)NLEJ193934531 DE-627 ger DE-627 rakwb eng On one technique for determining the spacecraft attitude prom the sun 1994 13 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Abstract A variant to implement a spacecraft (SC) spatial attitude system with respect to the Sun is discussed. The sunward direction and the solar rotation axis are used as reference points. The system is based on measuring spectral line Doppler shift by scanning the solar image along the limb and is self-adjusting for relative spectral line shifts and instrument band shifts. The first harmonic of the signal serves as a basis for accurate adjustment of filter band. The second harmonic phase is used to measure the spacecraft attitude. The application of this method holds the greatest promise when the SO is stabilized by the sunward spinning because this ensures continuous monitoring of the spacecraft attitude.In addition, the method provides information on the precise coordinates of solar surface details during space-borne observations. Springer Online Journal Archives 1860-2002 Kobanov, N. I. oth in Experimental astronomy 1989 5(1994) vom: März/Apr., Seite 301-313 (DE-627)NLEJ188994203 (DE-600)2012330-9 1572-9508 nnns volume:5 year:1994 month:03/04 pages:301-313 extent:13 http://dx.doi.org/10.1007/BF01583703 GBV_USEFLAG_U ZDB-1-SOJ GBV_NL_ARTICLE AR 5 1994 3/4 301-313 13 |
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(DE-627)NLEJ193934531 DE-627 ger DE-627 rakwb eng On one technique for determining the spacecraft attitude prom the sun 1994 13 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Abstract A variant to implement a spacecraft (SC) spatial attitude system with respect to the Sun is discussed. The sunward direction and the solar rotation axis are used as reference points. The system is based on measuring spectral line Doppler shift by scanning the solar image along the limb and is self-adjusting for relative spectral line shifts and instrument band shifts. The first harmonic of the signal serves as a basis for accurate adjustment of filter band. The second harmonic phase is used to measure the spacecraft attitude. The application of this method holds the greatest promise when the SO is stabilized by the sunward spinning because this ensures continuous monitoring of the spacecraft attitude.In addition, the method provides information on the precise coordinates of solar surface details during space-borne observations. Springer Online Journal Archives 1860-2002 Kobanov, N. I. oth in Experimental astronomy 1989 5(1994) vom: März/Apr., Seite 301-313 (DE-627)NLEJ188994203 (DE-600)2012330-9 1572-9508 nnns volume:5 year:1994 month:03/04 pages:301-313 extent:13 http://dx.doi.org/10.1007/BF01583703 GBV_USEFLAG_U ZDB-1-SOJ GBV_NL_ARTICLE AR 5 1994 3/4 301-313 13 |
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(DE-627)NLEJ193934531 DE-627 ger DE-627 rakwb eng On one technique for determining the spacecraft attitude prom the sun 1994 13 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Abstract A variant to implement a spacecraft (SC) spatial attitude system with respect to the Sun is discussed. The sunward direction and the solar rotation axis are used as reference points. The system is based on measuring spectral line Doppler shift by scanning the solar image along the limb and is self-adjusting for relative spectral line shifts and instrument band shifts. The first harmonic of the signal serves as a basis for accurate adjustment of filter band. The second harmonic phase is used to measure the spacecraft attitude. The application of this method holds the greatest promise when the SO is stabilized by the sunward spinning because this ensures continuous monitoring of the spacecraft attitude.In addition, the method provides information on the precise coordinates of solar surface details during space-borne observations. Springer Online Journal Archives 1860-2002 Kobanov, N. I. oth in Experimental astronomy 1989 5(1994) vom: März/Apr., Seite 301-313 (DE-627)NLEJ188994203 (DE-600)2012330-9 1572-9508 nnns volume:5 year:1994 month:03/04 pages:301-313 extent:13 http://dx.doi.org/10.1007/BF01583703 GBV_USEFLAG_U ZDB-1-SOJ GBV_NL_ARTICLE AR 5 1994 3/4 301-313 13 |
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On one technique for determining the spacecraft attitude prom the sun |
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Abstract A variant to implement a spacecraft (SC) spatial attitude system with respect to the Sun is discussed. The sunward direction and the solar rotation axis are used as reference points. The system is based on measuring spectral line Doppler shift by scanning the solar image along the limb and is self-adjusting for relative spectral line shifts and instrument band shifts. The first harmonic of the signal serves as a basis for accurate adjustment of filter band. The second harmonic phase is used to measure the spacecraft attitude. The application of this method holds the greatest promise when the SO is stabilized by the sunward spinning because this ensures continuous monitoring of the spacecraft attitude.In addition, the method provides information on the precise coordinates of solar surface details during space-borne observations. |
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Abstract A variant to implement a spacecraft (SC) spatial attitude system with respect to the Sun is discussed. The sunward direction and the solar rotation axis are used as reference points. The system is based on measuring spectral line Doppler shift by scanning the solar image along the limb and is self-adjusting for relative spectral line shifts and instrument band shifts. The first harmonic of the signal serves as a basis for accurate adjustment of filter band. The second harmonic phase is used to measure the spacecraft attitude. The application of this method holds the greatest promise when the SO is stabilized by the sunward spinning because this ensures continuous monitoring of the spacecraft attitude.In addition, the method provides information on the precise coordinates of solar surface details during space-borne observations. |
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Abstract A variant to implement a spacecraft (SC) spatial attitude system with respect to the Sun is discussed. The sunward direction and the solar rotation axis are used as reference points. The system is based on measuring spectral line Doppler shift by scanning the solar image along the limb and is self-adjusting for relative spectral line shifts and instrument band shifts. The first harmonic of the signal serves as a basis for accurate adjustment of filter band. The second harmonic phase is used to measure the spacecraft attitude. The application of this method holds the greatest promise when the SO is stabilized by the sunward spinning because this ensures continuous monitoring of the spacecraft attitude.In addition, the method provides information on the precise coordinates of solar surface details during space-borne observations. |
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