Optimal Orbit Transfer
Optimal Orbit Transfer is a spacecraft trajectory maneuver that belongs to the class of orbital transfer strategies, distinguished by its minimization of propellant consumption or delta-v requirement between two coplanar circular orbits under the two-body assumption.
113
Publications
4.1K
Citations
171
Authors
96
Institutions
Publications per year
2017–2026
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The Aerospace Corporation
El Segundo, United States
7 h-index
7 publications
177 citations

University of Pisa
Pisa, Italy
6 h-index
15 publications
317 citations
Jet Propulsion Laboratory
Pasadena, United States
6 h-index
9 publications
379 citations
University of Michigan
Ann Arbor, United States
5 h-index
9 publications
271 citations
University of Illinois Urbana-Champaign
Urbana, United States
5 h-index
7 publications
529 citations

Centre National de la Recherche Scientifique
Paris, France
4 h-index
7 publications
855 citations
University of Missouri
Columbia, United States
3 h-index
3 publications
98 citations
Institut de Recherche en Informatique de Toulouse
Toulouse, France
3 h-index
4 publications
195 citations
1–8 of 96
35 publications · 1.4K citations
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5 publications · 169 citations
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6 publications · 325 citations
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6 publications · 169 citations
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5 publications · 154 citations
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