Advantages of tether release of satellites from elliptic orbits

DOI10.2514/3.20337zbMath0657.70030OpenAlexW2134320992MaRDI QIDQ3806002

Bruce A. Conway, George A. Kyroudis

Publication date: 1988

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

Full work available at URL: https://doi.org/10.2514/3.20337

zbMATH Keywords

Lagrangian methodelliptically orbiting tethered-dumbbell (space shuttle-satellite)geosynchronous altitudetwo-dimensional rigid-body equations

Mathematics Subject Classification ID

Celestial mechanics (70F15) Orbital mechanics (70M20)

Related Items (1)

Dynamics and Control of Spinning Tethers for Rendezvous in Elliptic Orbits

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