Orbital Interception
Orbital Interception is a method in the field of relative motion that enables the precise determination and execution of a spacecraft trajectory to meet a target object in orbit by synchronizing their relative positions and velocities within a shared gravitational environment.
35
Publications
978
Citations
130
Authors
54
Institutions
Publications per year
2017–2026
15
Parents
35
1–5 of 35
130
3
h-index
2
h-index
2
h-index
2
h-index
2
h-index
1–5 of 130
54

National University of Defense Technology
Changsha, China
3 h-index
11 publications
235 citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
2 h-index
3 publications
163 citations
Massachusetts Institute of Technology
Cambridge, United States
2 h-index
11 publications
230 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
2 h-index
3 publications
74 citations

Harbin Institute of Technology
Harbin, China
2 h-index
9 publications
409 citations

Sun Yat-sen University
Guangzhou, China
2 h-index
3 publications
173 citations

Beijing Institute of Technology
Beijing, China
2 h-index
5 publications
233 citations

Mount Stromlo Observatory
Canberra, Australia
1 h-index
2 publications
72 citations
1–8 of 54
6 publications · 205 citations
6
h-index
4 publications · 135 citations
4
h-index
4 publications · 102 citations
4
h-index
AST · 3 publications · 99 citations
3
h-index
2 publications · 60 citations
2
h-index
1–5