Useful relative motion description method for perturbations analysis in satellite formation flying

DOI10.1007/BF03246253zbMath1170.70381MaRDI QIDQ957648

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

Publication date: 1 December 2008

Published in: Applied Mathematics and Mechanics. (English Edition) (Search for Journal in Brave)

zbMATH Keywords

rotation ratesatellite formation flyingdrift rategravitational perturbationrelative orbital element

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items

Approximate analysis for relative motion of satellite formation flying in elliptical orbits

Cites Work

• Study on relative orbital configuration in satellite formation flying
• Co‐ordination and control of distributed spacecraft systems using convex optimization techniques
• Dynamical behaviors and relative trajectories of the spacecraft formation flying
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