Floquet modes and stability analysis of periodic orbit-attitude solutions along Earth-Moon halo orbits

DOI10.1007/S10569-021-10030-YzbMath1472.70023OpenAlexW3183374524WikidataQ124828561 ScholiaQ124828561MaRDI QIDQ2049224

Michèle Lavagna, Francesco Colombi, Andrea Colagrossi

Publication date: 24 August 2021

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10569-021-10030-y

zbMATH Keywords

Floquet modesattitude manifoldsattitude stabilisationcircular restricted three-body problem (CR3BP)orbit-attitude dynamicsspin-stabilised spacecraft

Mathematics Subject Classification ID

Three-body problems (70F07) Stability for nonlinear problems in mechanics (70K20) Orbital mechanics (70M20)

Cites Work

• Fundamentals of spacecraft attitude determination and control
• Almost rectilinear halo orbits
• Three-dimensional, periodic, ?halo? orbits
• ELEMENTAL PERIODIC ORBITS ASSOCIATED WITH THE LIBRATION POINTS IN THE CIRCULAR RESTRICTED 3-BODY PROBLEM
• Attitude stability of a spinning symmetric satellite in a planar periodic orbit
• Attitude stability of a rigid body placed at an equilibrium point in the restricted problem of three bodies
• Attitude stability of a symmetric satellite at the equilibrium points in the restricted three-body problem
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