Time-optimal Trajectory Design
Time-Optimal Trajectory Design is a trajectory optimization framework within launch vehicle mission analysis that, as the nearest class, formulates ascent or orbital transfer paths as a mathematical problem of minimizing flight time, and, as the distinguishing characteristic, incorporates dynamic constraints, boundary conditions, and performance limits specific to launch vehicles to achieve the shortest feasible time-to-target while satisfying mission and physical feasibility requirements.
105
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4.5K
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284
Authors
134
Institutions
Publications per year
2017–2026
43
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Fang Zhou, Xiaopeng Li, Jiaqi Ma · Transportation Research Part B Methodological · 2016 · 222 citations
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Beijing Institute of Technology
Beijing, China
4 h-index
10 publications
364 citations
National University of Singapore
Singapore, Singapore
4 h-index
9 publications
1.4K citations
University of California, Los Angeles
Los Angeles, United States
2 h-index
3 publications
79 citations
Dalian University of Technology
Dalian, China
2 h-index
9 publications
420 citations

Peking University
Beijing, China
2 h-index
6 publications
534 citations
University of California, Santa Barbara
Santa Barbara, United States
2 h-index
2 publications
48 citations
Georgia Institute of Technology
Atlanta, United States
2 h-index
4 publications
85 citations
Carnegie Mellon University
Pittsburgh, United States
2 h-index
3 publications
449 citations
1–8 of 134
9 publications · 291 citations
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4 publications · 159 citations
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Repository · 3 publications · 40 citations
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2 publications · 92 citations
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IJRR · 2 publications · 262 citations
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