State Equations for a Spacecraft With Maneuvering Flexible Appendages in Terms of Quasi-Coordinates

DOI10.1115/1.3152387zbMath0761.70024OpenAlexW1980097764MaRDI QIDQ4015149

L. Meirovitch, Moon K. Kwak

Publication date: 14 December 1992

Published in: Applied Mechanics Reviews (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1115/1.3152387

zbMATH Keywords

spatial discretizationLagrange's equationsrigid platformspacecraft with a membrane-like antenna

Mathematics Subject Classification ID

Thin bodies, structures (74K99) Orbital mechanics (70M20)

Related Items (1)

Coupling dynamic analysis of spacecraft with multiple cylindrical tanks and flexible appendages

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