Launch Vehicle Trajectory Optimization
Launch Vehicle Trajectory Optimization is a computational framework within trajectory optimization that specifically addresses the determination of optimal flight paths for launch vehicles by balancing performance, safety, and vehicle constraints during ascent through atmospheric and orbital regimes.
165
Publications
5.2K
Citations
369
Authors
121
Institutions
Publications per year
2017–2026
40
Parents
165
1–5 of 165
369
10
h-index
9
h-index
6
h-index
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
4 publications · 68 citations
4
h-index
4
h-index
1–5 of 369
121

Beihang University
Beijing, China
13 h-index
35 publications
808 citations
Iowa State University
Ames, United States
11 h-index
20 publications
1.9K citations
Georgia Institute of Technology
Atlanta, United States
11 h-index
32 publications
913 citations

Langley Research Center
Hampton, United States
9 h-index
23 publications
856 citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
6 h-index
8 publications
255 citations

Northwestern Polytechnical University
Xi'an, China
6 h-index
14 publications
338 citations

Harbin Institute of Technology
Harbin, China
5 h-index
17 publications
511 citations
Marshall Space Flight Center
Redstone Arsenal, United States
5 h-index
7 publications
286 citations
1–8 of 121
25 publications · 1.6K citations
18
h-index
Conference · 15 publications · 405 citations
12
h-index
AST · 13 publications · 420 citations
12
h-index
13 publications · 327 citations
12
h-index
6 publications · 148 citations
6
h-index
1–5