Entry Trajectory Design
Entry Trajectory Design is a computational methodology within aerospace engineering that determines the optimal path and control profile for a spacecraft or entry vehicle during atmospheric entry, distinguishing itself from other mission design components by focusing specifically on the vehicle's flight trajectory from atmospheric interface to terminal phase, subject to constraints such as thermal loading, aerodynamic forces, and target accuracy.
112
Publications
4.3K
Citations
261
Authors
74
Institutions
Publications per year
2017–2026
31
Parents
112
1–5 of 112
261
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Langley Research Center
Hampton, United States
11 h-index
28 publications
1.4K citations

National University of Defense Technology
Changsha, China
9 h-index
37 publications
1.7K citations
Iowa State University
Ames, United States
9 h-index
14 publications
1.1K citations
Johnson Space Center
Houston, United States
7 h-index
11 publications
366 citations

Beihang University
Beijing, China
7 h-index
25 publications
744 citations
Georgia Institute of Technology
Atlanta, United States
6 h-index
19 publications
652 citations

Beijing Institute of Technology
Beijing, China
6 h-index
18 publications
855 citations

China Aerospace Science and Technology Corporation
Beijing, China
6 h-index
6 publications
213 citations
1–8 of 74
15 publications · 1K citations
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13 publications · 601 citations
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AST · 11 publications · 560 citations
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Conference · 10 publications · 300 citations
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Repository · 5 publications · 157 citations
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