J2-Perturbed Rendezvous is a spacecraft rendezvous model that accounts for the secular and periodic orbital perturbations caused by Earth's oblateness (J₂ term) in the gravitational potential, distinguishing it from simplified two-body rendezvous formulations by incorporating the dominant non-spherical gravitational effects on relative orbital motion.
11
Publications
455
Citations
31
Authors
15
Institutions
Publications per year
2017–2026
3
Parents
Publications
11
1–5 of 11
Authors
31
- HL
1
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- HB
1
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- XS
1
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- JZ
1
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- CL
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1–5 of 31
Institutions
15
Naval Postgraduate School
Monterey, United States
2 h-index
3 publications
302 citations
Shanghai Jiao Tong University
Shanghai, China
2 h-index
6 publications
129 citations
Shanghai Micro Satellite Engineering Center
Shanghai, China
1 h-index
1 publications
26 citations
European Space Research and Technology Centre
Noordwijk-Binnen, The Netherlands
1 h-index
1 publications
18 citations
University of Chinese Academy of Sciences
Beijing, China
1 h-index
1 publications
35 citations
Nanjing University of Aeronautics and Astronautics
Nanjing, China
1 h-index
3 publications
78 citations
Beihang University
Beijing, China
1 h-index
3 publications
60 citations
Tsinghua University
Beijing, China
1 h-index
3 publications
180 citations
1–8 of 15
Venues
- Acta Astronautica
3 publications · 113 citations
3
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- Journal of Guidance Control and Dynamics
3 publications · 243 citations
3
h-index
- Celestial Mechanics and Dynamical Astronomy
2 publications · 38 citations
2
h-index
- Aircraft Engineering and Aerospace Technology
1 publications · 17 citations
1
h-index
- Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering
1 publications · 18 citations
1
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1–5