Trajectory Phasing Analysis
Trajectory Phasing Analysis is a computational method used in interplanetary mission design that determines the optimal timing and orbital geometry for spacecraft departure and arrival to achieve desired trajectory characteristics while minimizing propellant consumption.
6
Publications
109
Citations
22
Authors
8
Institutions
Publications per year
2017–2026
3
Parents
6
DESTINY+ Trajectory Design to (3200) Phaethon
Bruno Sarli, Makoto Horikawa, Chit Hong Yam et al. · The Journal of the Astronautical Sciences · 2017 · 30 citations · Full text
Spacecraft long-duration phasing maneuver optimization using hybrid approach
Jin Zhang, Wang Xiang, MA Xiaobing et al. · Acta Astronautica · 2011 · 14 citations
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University of Siena
Siena, Italy
1 h-index
4 publications
44 citations
Japan Aerospace Exploration Agency
Tokyo, Japan
1 h-index
3 publications
90 citations

National University of Defense Technology
Changsha, China
1 h-index
2 publications
28 citations
University of Canberra
Canberra, Australia
1 h-index
6 publications
108 citations
China Academy of Space Technology
Beijing, China
1 h-index
3 publications
42 citations
Virginia Tech
Blacksburg, United States
1 h-index
2 publications
48 citations
UNSW Canberra
Canberra, Australia
1 h-index
6 publications
108 citations
Waseda University
Tokyo, Japan
1 h-index
1 publications
30 citations
1–8 of 8
2 publications · 35 citations
2
h-index
1 publications · 30 citations
1
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1 publications · 14 citations
1
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1 publications · 18 citations
1
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1 publications · 10 citations
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