Rendezvous Trajectory Design
Rendezvous Trajectory Design is a specialized method within spacecraft trajectory design that involves the systematic planning and optimization of a chaser spacecraft's path to safely and efficiently approach and meet a target spacecraft in orbit, distinguishing itself by incorporating relative motion dynamics, proximity operations constraints, and mission-specific objectives such as fuel minimization or time of flight.
152
Publications
5.1K
Citations
389
Authors
127
Institutions
Publications per year
2017–2026
54
152
1–5 of 152
389
5
h-index
5
h-index
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
4 publications · 177 citations
4
h-index
4
h-index
Johns Hopkins University Applied Physics Laboratory, United States
3 publications · 65 citations
3
h-index
1–5 of 389
127

Harbin Institute of Technology
Harbin, China
7 h-index
15 publications
374 citations

National University of Defense Technology
Changsha, China
7 h-index
19 publications
608 citations
Johnson Space Center
Houston, United States
5 h-index
7 publications
163 citations

Beijing Institute of Technology
Beijing, China
5 h-index
14 publications
267 citations
Tsinghua University
Beijing, China
5 h-index
16 publications
371 citations
Japan Aerospace Exploration Agency
Tokyo, Japan
5 h-index
26 publications
454 citations
Purdue University West Lafayette
West Lafayette, United States
4 h-index
8 publications
258 citations

University of Pisa
Pisa, Italy
4 h-index
9 publications
279 citations
1–8 of 127
23 publications · 1.3K citations
20
h-index
22 publications · 677 citations
18
h-index
17 publications · 528 citations
12
h-index
AST · 10 publications · 284 citations
10
h-index
6 publications · 151 citations
6
h-index
1–5