Optimal aeroassisted transfer between coplanar elliptical orbits

DOI10.1016/0094-5765(86)90084-6zbMath0598.70036OpenAlexW2018729314MaRDI QIDQ3733034

N. X. Vinh, Jennie R. Johannesen

Publication date: 1986

Published in: Acta Astronautica (Search for Journal in Brave)

Full work available at URL: http://hdl.handle.net/2027.42/26152

zbMATH Keywords

optimal rotationplanetary atmospherenearly circular orbitcomplete first-order solutioncoplanar elliptical orbitsdecelerative braking forceminimum-fuel, free-time transferoptimal pure propulsive two- impulse transfer

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

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