Three-body Trajectory Dynamics
Three-Body Trajectory Dynamics is a theoretical framework in astrodynamics that models the motion of a spacecraft under the gravitational influence of three celestial bodies, distinguishing itself from general trajectory models by explicitly accounting for the coupled nonlinear interactions and chaotic behavior arising from the restricted three-body problem.
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11.3K
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470
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282
Institutions
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2017–2026
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Connecting orbits and invariant manifolds in the spatial restricted three-body problem
Gérard Gómez, Wang Sang Koon, M. W. Lo et al. · Nonlinearity · 2004 · 312 citations
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Universitat Politècnica de Catalunya
Barcelona, Spain
9 h-index
18 publications
1.2K citations

Centre National de la Recherche Scientifique
Paris, France
8 h-index
19 publications
518 citations
University of Patras
Pátrai, Greece
8 h-index
17 publications
429 citations

Instituto Nacional de Pesquisas Espaciais
São José dos Campos, Brazil
8 h-index
12 publications
301 citations
Jet Propulsion Laboratory
Pasadena, United States
8 h-index
10 publications
703 citations
Aristotle University of Thessaloniki
Thessaloniki, Greece
8 h-index
8 publications
416 citations
University of Colorado Boulder
Boulder, United States
7 h-index
10 publications
258 citations
California Institute of Technology
Pasadena, United States
7 h-index
12 publications
1.8K citations
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43 publications · 1.3K citations
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13 publications · 613 citations
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15 publications · 404 citations
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13 publications · 316 citations
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AJ · 13 publications · 371 citations
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