Elliptical shape-based model for multi-revolution planeto-centric mission scenarios

DOI10.1007/S10569-020-10001-9zbMath1466.70038OpenAlexW3119090191MaRDI QIDQ2033670

Michelle Lavagna, Jacopo Prinetto

Publication date: 17 June 2021

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10569-020-10001-9

zbMATH Keywords

trajectory optimizationtrajectory designlow thrust

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Orbital mechanics (70M20)

Related Items (1)

Transfers from the Earth to \(L_2\) halo orbits in the Earth-Moon bicircular problem

Cites Work

• Survey of direct transcription for low-thrust space trajectory optimization with applications
• Unnamed Item
• Unnamed Item
• Unnamed Item

This page was built for publication: Elliptical shape-based model for multi-revolution planeto-centric mission scenarios