Osculating orbit

Results: 13



#Item
1Significance analysis of asteroid pairs  P. Pravec a, D. Vokrouhlick´y b, a Astronomical  Institute, Academy of Sciences of the Czech Republic, Friˇcova 1,

Significance analysis of asteroid pairs P. Pravec a, D. Vokrouhlick´y b, a Astronomical Institute, Academy of Sciences of the Czech Republic, Friˇcova 1,

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Source URL: www.asu.cas.cz

Language: English - Date: 2009-07-07 11:23:08
2APPENDIX B:  USING BROUWER-MEAN ELEMENTS FROM TBUS PART IV  The Brouwer-mean elements in part IV of the APT predict bulletin (TBUS) can be used in a

APPENDIX B: USING BROUWER-MEAN ELEMENTS FROM TBUS PART IV The Brouwer-mean elements in part IV of the APT predict bulletin (TBUS) can be used in a

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Source URL: www1.ncdc.noaa.gov

Language: English - Date: 2014-08-25 11:31:06
3Astrodynamics / Holism / Source code / Subroutine / University of Cambridge Computer Laboratory / Fortran / Osculating orbit / CN2 / Computer programming / Computing / Software engineering

APPENDIX F: Using Brouwer-mean elements from TBUS Part IV The Brouwer-mean elements in part IV of the APT predict bulletin (TBUS) can be used in a stand-alone Brouwer-Lyddane orbit prediction package to determine orbit

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Source URL: www1.ncdc.noaa.gov

Language: English - Date: 2013-08-21 14:36:11
4Proceedings of the 16th International Workshop on Laser Ranging  Preparing the Bernese GPS Software for the analysis of SLR observations to geodetic satellites D. Thaller (1), M. Mareyen (2), R. Dach (1), G. Beutler (1),

Proceedings of the 16th International Workshop on Laser Ranging Preparing the Bernese GPS Software for the analysis of SLR observations to geodetic satellites D. Thaller (1), M. Mareyen (2), R. Dach (1), G. Beutler (1),

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Source URL: cddis.gsfc.nasa.gov

Language: English - Date: 2010-01-20 16:12:02
5Geocenter Coordinates Estimated from a Combined Multi-GNSS Data Analysis Geocenter Coordinates Estimated from GPS and GLONASS Data In our analysis each orbit is parameterized with six osculating orbital elements (semi-ma

Geocenter Coordinates Estimated from a Combined Multi-GNSS Data Analysis Geocenter Coordinates Estimated from GPS and GLONASS Data In our analysis each orbit is parameterized with six osculating orbital elements (semi-ma

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Source URL: www.bernese.unibe.ch

Language: English - Date: 2012-05-04 03:18:15
6ON THE THEORY OF CANONICAL PERTURBATIONS AND ITS APPLICATIONS TO EARTH ROTATION: A SOURCE OF INACCURACY IN THE CALCULATION OF ANGULAR VELOCITY M. EFROIMSKY US Naval Observatory Washington DC[removed]USA

ON THE THEORY OF CANONICAL PERTURBATIONS AND ITS APPLICATIONS TO EARTH ROTATION: A SOURCE OF INACCURACY IN THE CALCULATION OF ANGULAR VELOCITY M. EFROIMSKY US Naval Observatory Washington DC[removed]USA

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Source URL: aa.usno.navy.mil

Language: English - Date: 2014-11-21 14:29:23
7Celestial Mech Dyn Astr[removed]:261–292 DOI[removed]s10569[removed]ORIGINAL ARTICLE Long-term evolution of orbits about a precessing oblate planet: 3. A semianalytical and a purely numerical

Celestial Mech Dyn Astr[removed]:261–292 DOI[removed]s10569[removed]ORIGINAL ARTICLE Long-term evolution of orbits about a precessing oblate planet: 3. A semianalytical and a purely numerical

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Source URL: aa.usno.navy.mil

Language: English - Date: 2014-11-21 14:29:25
8The theory of canonical perturbations applied to attitude dynamics and to the Earth rotation. Osculating and nonosculating Andoyer variables. Michael Efroimsky  arXiv:astro-ph/0506427v6 17 Jul 2007

The theory of canonical perturbations applied to attitude dynamics and to the Earth rotation. Osculating and nonosculating Andoyer variables. Michael Efroimsky arXiv:astro-ph/0506427v6 17 Jul 2007

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Source URL: aa.usno.navy.mil

Language: English - Date: 2014-11-21 14:29:24
9Celestial Mech Dyn Astr[removed]:259–288 DOI[removed]s10569[removed]O R I G I NA L A RT I C L E Long-term evolution of orbits about a precessing oblate planet. 2. The case of variable precession∗

Celestial Mech Dyn Astr[removed]:259–288 DOI[removed]s10569[removed]O R I G I NA L A RT I C L E Long-term evolution of orbits about a precessing oblate planet. 2. The case of variable precession∗

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Source URL: aa.usno.navy.mil

Language: English - Date: 2014-11-21 14:29:23
10LONG-TERM EVOLUTION OF ORBITS ABOUT A PRECESSING OBLATE PLANET: 1. THE CASE OF UNIFORM PRECESSION1 MICHAEL EFROIMSKY US Naval Observatory, Washington DC 20392, USA, e-mail: [removed]  (Received: 19 July 2004; revi

LONG-TERM EVOLUTION OF ORBITS ABOUT A PRECESSING OBLATE PLANET: 1. THE CASE OF UNIFORM PRECESSION1 MICHAEL EFROIMSKY US Naval Observatory, Washington DC 20392, USA, e-mail: [removed] (Received: 19 July 2004; revi

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Source URL: aa.usno.navy.mil

Language: English - Date: 2014-11-21 14:29:23