Flexible Spacecraft Coupling
Flexible Spacecraft Coupling is a dynamic interaction phenomenon in astrodynamics wherein the elastic deformations of a spacecraft's flexible structural components directly influence and are influenced by its orbital and attitude motion, thereby distinguishing it from rigid-body spacecraft coupling through the inclusion of structural flexibility effects in the coupled attitude-orbit dynamics.
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1.7K
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2017–2026
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On-orbit assembly of a team of flexible spacecraft using potential field based method
Ti Chen, Hao Wen, Haiyan Hu et al. · Acta Astronautica · 2017 · 62 citations
Stability of flexible spacecrafts
P. Santini · Acta Astronautica · 1976 · 61 citations
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Harbin Institute of Technology
Harbin, China
9 h-index
26 publications
763 citations

Beijing Institute of Technology
Beijing, China
8 h-index
19 publications
706 citations
Dalian University of Technology
Dalian, China
3 h-index
9 publications
213 citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
3 h-index
11 publications
434 citations
Toronto Metropolitan University
Toronto, Canada
3 h-index
3 publications
108 citations
Virginia Tech
Blacksburg, United States
3 h-index
5 publications
239 citations

York University
Toronto, Canada
2 h-index
5 publications
126 citations
China Academy of Space Technology
Beijing, China
2 h-index
5 publications
60 citations
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12 publications · 471 citations
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6 publications · 188 citations
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AST · 2 publications · 76 citations
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