Dynamics of a Spacecraft during Extension of Flexible Appendages

DOI10.2514/3.56343zbMath0521.70030OpenAlexW2072875724MaRDI QIDQ3670648

Kazuo Tsuchiya

Publication date: 1983

Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.56343

zbMATH Keywords

method of multiple scalesattitude behavior of spacecraft with rotorextension of flexible appendagesmodal coordinate scheme

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Control of mechanical systems (70Q05) Astronomy and astrophysics (85A99) Orbital mechanics (70M20)

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