Analysis of dynamics and control during the deployment of an annular tether group of spacecraft

DOI10.3103/s0025654422601549MaRDI QIDQ6147214

Yu. M. Zabolotnov, Asiya A. Nazarova, Ch. Wang

Publication date: 15 January 2024

Published in: Mechanics of Solids (Search for Journal in Brave)

zbMATH Keywords

Lagrange equationsreactive forceexternal torquelow-thrust engineregular polygon configurationring tether grouping

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Cites Work

• Three-dimensional multi-tethered satellite formation with the elements moving along Lissajous curves
• Analysis of the dynamics of the formation of a tether group of three nanosatellites taking into account their motion around the centers of mass

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