Analytical method for the attitude stability of partially liquid filled spacecraft with flexible appendage

DOI10.1007/s10409-016-0616-9zbMath1365.70028OpenAlexW2556759664MaRDI QIDQ2359643

Yulong Yan, Bao-Zeng Yue

Publication date: 22 June 2017

Published in: Acta Mechanica Sinica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10409-016-0616-9

zbMATH Keywords

stability analysisenergy-Casimir methodliquid-filled spacecraftflexible attachment

Mathematics Subject Classification ID

Rods (beams, columns, shafts, arches, rings, etc.) (74K10) Orbital mechanics (70M20)

Related Items (1)

Study on the dynamics, relative equilibria, and stability for liquid-filled spacecraft with flexible appendage

Cites Work

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• Steady rotation of a composite sphere in a concentric spherical cavity
• Coupling dynamic analysis of a liquid-filled spherical container subject to arbitrary excitation
• Heteroclinic bifurcations in attitude maneuver of coupled slosh-spacecraft with flexible appendage
• Hamiltonian structures and stability for rigid bodies with flexible attachments
• Coupling dynamic analysis of spacecraft with multiple cylindrical tanks and flexible appendages
• The numerical simulation of liquid sloshing on board spacecraft
• Stabilization of rigid body dynamics by the Energy-Casimir method
• Attitude dynamics of a liquid-filled spacecraft with a manipulator
• Stability of a spinning liquid-filled spacecraft
• Nonlinear stability of fluid and plasma equilibria
• Liquid Sloshing Dynamics
• STABILITY BOUNDARIES OF LIQUID-PROPELLED SPACE VEHICLES WITH SLOSHING

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