Low-thrust trajectory optimization in a full ephemeris model

DOI10.1007/S10409-014-0038-5zbMath1346.70026OpenAlexW2059209447MaRDI QIDQ318431

Mohammad Hasan, M. Dambrine

Publication date: 5 October 2016

Published in: Acta Mechanica Sinica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10409-014-0038-5

zbMATH Keywords

full ephemeris modelgravity assistlow-thrust

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Uses Software

• OTIS

Cites Work

• Conversion of Optimal Control Problems into Parameter Optimization Problems
• Direct trajectory optimization using nonlinear programming and collocation
• Discrete approximations to optimal trajectories using direct transcription and nonlinear programming
• Optimal Low-Earth-Orbit-Geostationary-Earth-Orbit Intermediate Acceleration Orbit Transfer
• Powered swingby

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