Ascent Trajectory Optimization
Ascent Trajectory Optimization is a computational methodology within launch vehicle trajectory analysis that determines the optimal control and path parameters during the powered ascent phase to minimize fuel consumption, maximize payload delivery, or satisfy mission-specific constraints while adhering to dynamic, aerodynamic, and gravitational forces.
96
Publications
3K
Citations
238
Authors
77
Institutions
Publications per year
2017–2026
28
96
Rapid Optimal Multiburn Ascent Planning and Guidance
Ping Lu, Brian Griffin, Gregory A. Dukeman et al. · Journal of Guidance Control and Dynamics · 2008 · 108 citations
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Georgia Institute of Technology
Atlanta, United States
8 h-index
16 publications
746 citations

Beihang University
Beijing, China
8 h-index
16 publications
534 citations

Northwestern Polytechnical University
Xi'an, China
7 h-index
10 publications
348 citations

Langley Research Center
Hampton, United States
6 h-index
15 publications
291 citations
Iowa State University
Ames, United States
6 h-index
14 publications
1K citations
Marshall Space Flight Center
Redstone Arsenal, United States
5 h-index
6 publications
199 citations

Sapienza University of Rome
Rome, Italy
5 h-index
16 publications
569 citations

Ames Research Center
Mountain View, United States
4 h-index
5 publications
102 citations
1–8 of 77
19 publications · 1.2K citations
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AST · 10 publications · 310 citations
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8 publications · 165 citations
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Conference · 6 publications · 131 citations
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3 publications · 92 citations
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