Fuel-Optimal Rendezvous is a spacecraft trajectory optimization method that belongs to the class of orbital rendezvous strategies and is distinguished by its objective of minimizing propellant consumption during the approach and docking or proximity operations between two space vehicles.
54
Publications
2.2K
Citations
99
Authors
50
Institutions
Publications per year
2017–2026
7
Parents
Publications
54
Optimum low-thrust rendezvous and station keeping
T. N. Edelbaum · AIAA Journal · 1964 · 90 citations
1–5 of 54
Authors
99
- FY
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- JP
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- LB
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- DADenis Arzelier
Laboratoire d'Analyse et d'Architecture des Systèmes, France
3 publications · 63 citations
3
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- TE
3
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1–5 of 99
Institutions
50
Eastern Connecticut State University
Willimantic, United States
6 h-index
6 publications
375 citations
Jet Propulsion Laboratory
Pasadena, United States
6 h-index
9 publications
160 citations
Massachusetts Institute of Technology
Cambridge, United States
4 h-index
8 publications
570 citations
Tsinghua University
Beijing, China
4 h-index
12 publications
243 citations
Worcester Polytechnic Institute
Worcester, United States
4 h-index
4 publications
309 citations
Brigham Young University
Provo, United States
3 h-index
4 publications
78 citations
Université Fédérale de Toulouse Midi-Pyrénées
Toulouse, France
3 h-index
7 publications
163 citations
Georgia Institute of Technology
Atlanta, United States
2 h-index
3 publications
90 citations
1–8 of 50
Venues
- Journal of Guidance Control and Dynamics
20 publications · 1.1K citations
18
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- AIAA Journal
6 publications · 349 citations
6
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- AIAA Guidance, Navigation, and Control Conference and Exhibit
Conference · 3 publications · 96 citations
3
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- Advances in Space Research
2 publications · 48 citations
2
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- Journal of Spacecraft and Rockets
2 publications · 38 citations
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1–5