Reentry Trajectory Estimation
Reentry Trajectory Estimation is a computational method within orbit determination that specifically characterizes the path of a space object during atmospheric reentry by integrating dynamic models with observational data to predict its position, velocity, and flight conditions from the initial atmospheric interface to impact or landing.
31
Publications
894
Citations
85
Authors
36
Institutions
Publications per year
2017–2026
10
Parents
31
1–5 of 31
85
2
h-index
2
h-index
Istituto di Scienza e Tecnologie dell'Informazione "Alessandro Faedo", Italy
1 publications · 33 citations
1
h-index
1
h-index
1
h-index
1–5 of 85
36

Harbin Institute of Technology
Harbin, China
2 h-index
4 publications
145 citations
Japan Aerospace Exploration Agency
Tokyo, Japan
2 h-index
2 publications
50 citations
Tianjin University
Tianjin, China
2 h-index
5 publications
336 citations

Northwestern Polytechnical University
Xi'an, China
2 h-index
6 publications
189 citations

National University of Defense Technology
Changsha, China
2 h-index
2 publications
28 citations
RTX (United States)
Arlington, United States
2 h-index
2 publications
36 citations
National Central University
Taoyuan City, Taiwan
2 h-index
2 publications
50 citations
Air Force Engineering University
Xi'an, China
1 h-index
3 publications
108 citations
1–8 of 36
4 publications · 113 citations
4
h-index
4 publications · 171 citations
4
h-index
3 publications · 58 citations
3
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AST · 2 publications · 70 citations
2
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2 publications · 193 citations
2
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1–5