Nonlinear Attitude-orbit Interaction
Nonlinear Attitude-Orbit Interaction is a theoretical framework in astrodynamics that characterizes the bidirectional, nonlinear coupling between a spacecraft's rotational dynamics and its orbital motion, where the attitude evolution induces non-negligible perturbations on the trajectory and vice versa, deviating significantly from decoupled or linearized models.
25
Publications
609
Citations
61
Authors
36
Institutions
Publications per year
2017–2026
9
Variants
Nonlinear Attitude-orbit Coupling
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36

Shanghai Jiao Tong University
Shanghai, China
3 h-index
6 publications
91 citations
Purdue University West Lafayette
West Lafayette, United States
2 h-index
2 publications
60 citations

Sharif University of Technology
Tehran, Iran
2 h-index
3 publications
64 citations

Shanghai University
Shanghai, China
2 h-index
2 publications
32 citations

Harbin Institute of Technology
Harbin, China
2 h-index
3 publications
101 citations

Beihang University
Beijing, China
2 h-index
2 publications
86 citations
Nanyang Technological University
Singapore, Singapore
2 h-index
3 publications
93 citations

Indian Institute of Science Bangalore
Bengaluru, India
1 h-index
1 publications
53 citations
1–8 of 36
5 publications · 109 citations
5
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AST · 3 publications · 94 citations
3
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3 publications · 52 citations
3
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2 publications · 33 citations
2
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JSV · 2 publications · 88 citations
2
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1–5