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Study on relative orbital configuration in satellite formation flying

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Publication:608580
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DOI10.1007/s10409-004-0009-3zbMath1200.70030OpenAlexW1986486603MaRDI QIDQ608580

Xin Meng, Xiang Li, Jun-Feng Li, Yun-Feng Gao

Publication date: 25 November 2010

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

Full work available at URL: https://doi.org/10.1007/s10409-004-0009-3

zbMATH Keywords

simulationperturbationsatellite formation flyingorbital elementrelative orbital configuration


Mathematics Subject Classification ID

Orbital mechanics (70M20)


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Influence of flexible solar arrays on vibration isolation platform of control moment gyroscopes, Attitude control for part actuator failure of agile small satellite, Approximate analysis for relative motion of satellite formation flying in elliptical orbits, Formation reconfiguration in restricted three body problem, \(J _{2}\) invariant relative orbits via differential correction algorithm, Orbit and attitude control of spacecraft formation flying, Useful relative motion description method for perturbations analysis in satellite formation flying, Adaptive control for autonomous rendezvous of spacecraft on elliptical orbit



Cites Work

  • Dynamical behaviors and relative trajectories of the spacecraft formation flying
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