Two-body Orbit Dynamics
Two-Body Orbit Dynamics is a mathematical model in orbital mechanics that describes the motion of a spacecraft or celestial body under the influence of gravitational attraction from a single primary body, assuming no perturbations from other forces or bodies.
17
Publications
1.8K
Citations
47
Authors
40
Institutions
Publications per year
2017–2026
6
Parents
17
Studies of nearby poor clusters - A3574 and S753
Christopher N. A. Willmer, P. Focardi, R. Chan et al. · The Astronomical Journal · 1991 · 51 citations
Natural Sciences, Astronomy, Physics +11
1–5 of 17
47
National Research Institute of Astronomy and Geophysics, Egypt
1 publications · 14 citations
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1
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1–5 of 47
40

Centre National de la Recherche Scientifique
Paris, France
2 h-index
2 publications
73 citations
Stony Brook University
Stony Brook, United States
1 h-index
1 publications
23 citations
Flatiron Institute
New York, United States
1 h-index
1 publications
23 citations

Netaji Subhas University of Technology
New Delhi, India
1 h-index
2 publications
58 citations
Université Paris Cité
Paris, France
1 h-index
1 publications
41 citations

Université Côte d'Azur
Nice, France
1 h-index
1 publications
32 citations

Cornell University
Ithaca, United States
1 h-index
1 publications
59 citations
William & Mary
Williamsburg, United States
1 h-index
2 publications
68 citations
1–8 of 40
2 publications · 42 citations
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2 publications · 69 citations
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2 publications · 38 citations
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1 publications · 32 citations
1
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1 publications · 16 citations
1
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