Attitude dynamics of three-body tethered systems

DOI10.1016/0094-5765(88)90189-0zbMath0657.70029OpenAlexW1981673606MaRDI QIDQ3806000

V. J. Modi, Arun K. Misra, Z. Amier

Publication date: 1988

Published in: Acta Astronautica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0094-5765(88)90189-0

zbMATH Keywords

dynamic responseequilibrium configurationsorbital planedouble-pendulumtether-connected three-body systemthree-body constellation

Mathematics Subject Classification ID

Three-body problems (70F07) Orbital mechanics (70M20)

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Equilibrium configurations of the tethered three-body formation system and their nonlinear dynamics ⋮ Nonlinear dynamic analysis of a three-body tethered satellite system with deployment/retrieval ⋮ Parametric stability of a double pendulum with variable length and with its center of mass in an elliptic orbit ⋮ Unnamed Item ⋮ Dynamics of a flexible multi-tethered satellite formation in a halo orbit with uncertain parameters ⋮ Dynamics and control of multi-connected satellites aligned along local horizontal

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