Heteroclinic bifurcations in attitude maneuver of coupled slosh-spacecraft with flexible appendage

DOI10.1007/S11431-011-4476-ZzbMath1237.70021OpenAlexW1576586126MaRDI QIDQ413098

Xiao-Juan Song, Bao-Zeng Yue

Publication date: 4 May 2012

Published in: Science China. Technological Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11431-011-4476-z

zbMATH Keywords

chaoticliquid-filled spacecraftliquid sloshattitude maneuverflexible appendage

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Bifurcations of singular points in dynamical systems (37G10) Strange attractors, chaotic dynamics of systems with hyperbolic behavior (37D45) Dynamics of multibody systems (70E55)

Related Items (9)

Analytical method for the attitude stability of partially liquid filled spacecraft with flexible appendage ⋮ Attitude tracking control of flexible spacecraft with large amplitude slosh ⋮ Attitude evolution of a dual-liquid-filled spacecraft with internal energy dissipation ⋮ Integrated vibration suppression attitude control for flexible spacecrafts with internal liquid sloshing ⋮ Chaos analysis in attitude dynamics of a flexible satellite ⋮ Coupling dynamic analysis of spacecraft with multiple cylindrical tanks and flexible appendages ⋮ Attitude dynamics of coupled spacecraft undergoing fuel transfer ⋮ Study on the dynamics, relative equilibria, and stability for liquid-filled spacecraft with flexible appendage ⋮ Study on the coupled dynamics of rigid-liquid-flexible spacecraft by using isogeometric analysis for liquid sloshing

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