Coupling dynamic analysis of spacecraft with multiple cylindrical tanks and flexible appendages

DOI10.1007/S10409-015-0497-3zbMath1342.70068OpenAlexW2238753393MaRDI QIDQ739974

Bao-Zeng Yue, Hua Huang, Wen-tsün Wu

Publication date: 11 August 2016

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

Full work available at URL: https://doi.org/10.1007/s10409-015-0497-3

zbMATH Keywords

Fourier-Bessel series expansion methodLagrange's equations in terms of quasi-coordinateslow-gravity environmentmaneuvering flexible appendagesmultiple liquid-filled cylindrical tanks

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items (2)

Analytical method for the attitude stability of partially liquid filled spacecraft with flexible appendage ⋮ Attitude tracking control of flexible spacecraft with large amplitude slosh

Cites Work

• Unnamed Item
• Unnamed Item
• Chaotic attitude and reorientation maneuver for completely liquid-filled spacecraft with flexible appendage
• Heteroclinic bifurcations in attitude maneuver of coupled slosh-spacecraft with flexible appendage
• Study on the global chaotic dynamics and control of liquid-filled spacecraft with flexible appendage
• Nonlinear coupled dynamics of liquid-filled spherical container in microgravity
• Attitude maneuver of liquid-filled spacecraft with a flexible appendage by momentum wheel
• Equations of motion for maneuvering flexible spacecraft
• State Equations for a Spacecraft With Maneuvering Flexible Appendages in Terms of Quasi-Coordinates
• Liquid Sloshing Dynamics

This page was built for publication: Coupling dynamic analysis of spacecraft with multiple cylindrical tanks and flexible appendages