Orbital maneuvers using low thrust to place a satellite in a constellation

DOI10.1155/2007/98532zbMath1141.70013OpenAlexW1978705091WikidataQ114842730 ScholiaQ114842730MaRDI QIDQ936187

Antonio Fernando Bertachini De Almeida Prado, Vivian Martins Gomes, Hélio Koiti Kuga

Publication date: 13 August 2008

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://eudml.org/doc/54359

zbMATH Keywords

Keplerian elementsminimum fuel consumption

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Cites Work

• Optimal Low-Earth-Orbit-Geostationary-Earth-Orbit Intermediate Acceleration Orbit Transfer
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