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

DOI10.2514/2.4116zbMath0885.70020OpenAlexW2056341651MaRDI QIDQ4355563

Jean Albert Kéchichian

Publication date: 22 April 1998

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

Full work available at URL: https://doi.org/10.2514/2.4116

zbMATH Keywords

integrationaveragingminimum-time orbit transfer

Mathematics Subject Classification ID

Orbital mechanics (70M20)

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Low-thrust trajectory optimization in a full ephemeris model ⋮ Reaction control system optimization for maneuverable reentry vehicles based on particle swarm optimization ⋮ Orbital maneuvers using low thrust to place a satellite in a constellation ⋮ Using Homotopy Method to Solve Bang–Bang Optimal Control Problems

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