A Multi-Revolution Lambert Solution is a specialized orbital mechanics algorithm within the class of Lambert's problem solvers that uniquely enables the determination of transfer trajectories involving multiple full revolutions around the central body before rendezvous, distinguishing it from conventional single-revolution solutions by accounting for extended flight paths and complex periodic boundary conditions.
14
Publications
602
Citations
26
Authors
10
Institutions
Publications per year
2017–2026
3
Variants
Multi-revolution Lambert's Problem Solution
Parents
Publications
14
1–5 of 14
Authors
26
- GZ
3
h-index
- CO
2
h-index
- DM
2
h-index
- RP
2
h-index
- PT
2
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1–5 of 26
Institutions
10
Texas A&M University
College Station, United States
3 h-index
7 publications
254 citations
Harbin Institute of Technology
Harbin, China
3 h-index
4 publications
172 citations
The University of Texas at Austin
Austin, United States
2 h-index
4 publications
98 citations
Georgia Institute of Technology
Atlanta, United States
2 h-index
4 publications
282 citations
Defence Institute of Advanced Technology
Pune, India
1 h-index
2 publications
54 citations
Universidad Politécnica de Madrid
Madrid, Spain
1 h-index
3 publications
72 citations
University of Illinois Urbana-Champaign
Urbana, United States
1 h-index
1 publications
109 citations
Beihang University
Beijing, China
1 h-index
3 publications
93 citations
1–8 of 10
Venues
- Journal of Guidance Control and Dynamics
9 publications · 399 citations
9
h-index
- The Journal of the Astronautical Sciences
2 publications · 133 citations
2
h-index
- Advanced Maui Optical and Space Surveillance Technologies Conference
Conference · 1 publications · 11 citations
1
h-index
- Celestial Mechanics and Dynamical Astronomy
1 publications · 46 citations
1
h-index
- AIAA Guidance, Navigation, and Control Conference and Exhibit
Conference · 1 publications · 13 citations
1
h-index
1–5