Fuel-optimal Trajectories
Fuel-Optimal Trajectories is a trajectory optimization method that determines the minimum propellant consumption path for orbital transfers by leveraging impulsive maneuvers at apoapsis and periapsis, distinguishing it from other trajectory designs through its adherence to the principles of the Hohmann transfer as the most fuel-efficient two-impulse solution in coplanar circular orbits.
162
Publications
7.4K
Citations
356
Authors
137
Institutions
Publications per year
2017–2026
47
Parents
162
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Jet Propulsion Laboratory
Pasadena, United States
13 h-index
40 publications
1.8K citations
Tsinghua University
Beijing, China
12 h-index
38 publications
2.5K citations
Virginia Tech
Blacksburg, United States
7 h-index
14 publications
580 citations
Massachusetts Institute of Technology
Cambridge, United States
7 h-index
17 publications
2.8K citations
The University of Texas at Austin
Austin, United States
6 h-index
11 publications
966 citations

Beihang University
Beijing, China
6 h-index
13 publications
416 citations
University of Michigan
Ann Arbor, United States
6 h-index
9 publications
421 citations

Linköping University
Linköping, Sweden
5 h-index
14 publications
1.1K citations
1–8 of 137
49 publications · 3.1K citations
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9 publications · 305 citations
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5 publications · 229 citations
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6 publications · 309 citations
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Conference · 4 publications · 189 citations
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