General formulation for N-body tethered satellite system dynamics

DOI10.2514/3.21582zbMath0867.70018OpenAlexW2031226679MaRDI QIDQ4896876

V. J. Modi, Arun K. Misra, Mehdi Keshmiri

Publication date: 22 October 1996

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

Full work available at URL: https://doi.org/10.2514/3.21582

zbMATH Keywords

controllinearizationeigenvalue analysishigher frequenciesassumed-mode methodlarge librational motionsegmented-tether modelvariable lengths

Mathematics Subject Classification ID

Orbital mechanics (70M20) Lagrange's equations (70H03)

Related Items (4)

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 ⋮ Vibration and elastic wave propagation in spatial flexible damping panel attached to four special springs ⋮ Dynamic modeling of cable system using a new nodal position finite element method

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