Capture Trajectories
"Capture Trajectory" is a conic section orbit that represents a two-body orbital motion solution wherein a spacecraft approaches a celestial body along a hyperbolic trajectory and employs a maneuver or natural perturbation to transition into a bounded elliptical orbit, distinguishing it from other transfer or flyby trajectories by achieving orbital capture.
56
Publications
1.8K
Citations
121
Authors
57
Institutions
Publications per year
2017–2026
13
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1–5 of 56
121
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57
Purdue University West Lafayette
West Lafayette, United States
6 h-index
14 publications
412 citations
Jet Propulsion Laboratory
Pasadena, United States
5 h-index
8 publications
413 citations

University of Glasgow
Glasgow, United Kingdom
3 h-index
5 publications
79 citations
California Institute of Technology
Pasadena, United States
3 h-index
4 publications
307 citations
Universidade Estadual Paulista (Unesp)
São Paulo, Brazil
3 h-index
3 publications
51 citations
Tsinghua University
Beijing, China
2 h-index
3 publications
137 citations
University of Missouri
Columbia, United States
2 h-index
2 publications
98 citations

Chinese Academy of Sciences
Beijing, China
2 h-index
4 publications
88 citations
1–8 of 57
13 publications · 376 citations
12
h-index
5 publications · 134 citations
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4 publications · 144 citations
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2 publications · 40 citations
3
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2 publications · 69 citations
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1–5