Dynamics of a tethered satellite in elliptical, non-equatorial orbits

DOI10.2514/3.20883zbMath0759.70019OpenAlexW2081628732MaRDI QIDQ4014647

Guido de Matteis

Publication date: 18 October 1992

Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.20883

zbMATH Keywords

linear stabilityenergy transferparametric resonanceeccentricityinclinationequatorial orbitsforced resonance

Mathematics Subject Classification ID

Stability for nonlinear problems in mechanics (70K20) Orbital mechanics (70M20)

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