Coordinate transformation and truncation for rotating spacecraft with flexible appendages
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Publication:4114843
DOI10.2514/3.7042zbMath0345.73059OpenAlexW2115006187MaRDI QIDQ4114843
Peter W. Likins, Yoshiaki Ohkami
Publication date: 1976
Published in: AIAA Journal (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.2514/3.7042
Finite element methods applied to problems in solid mechanics (74S05) Thin bodies, structures (74K99) Modal analysis in linear vibration theory (70J10) Orbital mechanics (70M20) Linear vibration theory (70J99) Numerical linear algebra (65F99)
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