Attitude-orbit Coupling
Attitude-Orbit Coupling is a dynamical interaction in astrodynamics wherein the rotational motion of a celestial body or artificial satellite influences and is influenced by its translational trajectory through gravitational and perturbative forces.
398
Publications
13.9K
Citations
925
Authors
329
Institutions
Publications per year
2017–2026
100
Variants
Attitude-orbit InteractionCoupled Attitude-orbit Dynamics
Parents
398
On the attitude stabilization of rigid spacecraft
Christopher I. Byrnes, Alberto Isidori · Automatica · 1991 · 289 citations
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329

Beihang University
Beijing, China
12 h-index
30 publications
1K citations

Harbin Institute of Technology
Harbin, China
12 h-index
34 publications
1.1K citations
Japan Aerospace Exploration Agency
Tokyo, Japan
12 h-index
60 publications
2.4K citations

Northwestern Polytechnical University
Xi'an, China
10 h-index
17 publications
506 citations
University of Michigan
Ann Arbor, United States
10 h-index
44 publications
2.7K citations
Jet Propulsion Laboratory
Pasadena, United States
9 h-index
28 publications
2.8K citations
University of Colorado Boulder
Boulder, United States
9 h-index
18 publications
431 citations
Keldysh Institute of Applied Mathematics
Moscow, Russia
9 h-index
17 publications
536 citations
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57 publications · 1.5K citations
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31 publications · 2K citations
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24 publications · 680 citations
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21 publications · 763 citations
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AST · 20 publications · 546 citations
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