Orbital Element Variations is a dynamical construct that represents the time-dependent deviations in the six classical orbital elements (semi-major axis, eccentricity, inclination, longitude of the ascending node, argument of periapsis, and true anomaly) of a celestial body or artificial satellite due to perturbative forces acting upon its trajectory.
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The ELODIE survey for northern extra-solar planets
D. Naef, M. Mayor, Jean-Luc Beuzit et al. · Astronomy and Astrophysics · 2004 · 125 citations · Full text
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Université Joseph Fourier
Grenoble, France
4 h-index
9 publications
732 citations
Observatoire Cantonal de Neuchâtel
Neuchâtel, Switzerland
4 h-index
18 publications
1.5K citations
Université Grenoble Alpes
Saint-Martin-d'Hères, France
3 h-index
6 publications
480 citations
Centre National de la Recherche Scientifique
Paris, France
3 h-index
3 publications
55 citations
Observatoire de Haute-Provence
Avignon, France
3 h-index
3 publications
240 citations
NSF National Center for Atmospheric Research
Boulder, United States
3 h-index
4 publications
403 citations
The University of Adelaide
Adelaide, Australia
2 h-index
3 publications
237 citations
Jet Propulsion Laboratory
Pasadena, United States
2 h-index
4 publications
93 citations
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- The Astronomical Journal
AJ · 5 publications · 370 citations
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- Celestial Mechanics and Dynamical Astronomy
4 publications · 254 citations
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- Astronomy and Astrophysics
4 publications · 324 citations
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- Monthly Notices of the Royal Astronomical Society
4 publications · 241 citations
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- The Astrophysical Journal
ApJ · 3 publications · 163 citations
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