Floquet-based design and control approach to spacecraft formation flying in libration point orbits

DOI10.1007/s11431-010-4250-7zbMath1241.70040OpenAlexW2021195175MaRDI QIDQ546585

YueDong Zhang, JinHai Dai, Yun-He Meng

Publication date: 24 June 2011

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

Full work available at URL: https://doi.org/10.1007/s11431-010-4250-7

zbMATH Keywords

spacecraft formationFloquet mode

Mathematics Subject Classification ID

Three-body problems (70F07) Orbital mechanics (70M20)

Related Items (1)

A novel method of periodic orbit computation in circular restricted three-body problem

Cites Work

• Natural and non-natural spacecraft formations near the L₁and L₂libration points in the Sun–Earth/Moon ephemeris system
• New approach to halo orbit determination and control
• ELEMENTAL PERIODIC ORBITS OF THE CR3BP: A BRIEF SELECTION OF COMPUTATIONAL RESULTS

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