Using a three-impulse maneuvering scheme for returning from the lunar orbit to the reentry point of the Earth's atmosphere

DOI10.1134/S1064230720010050zbMath1453.93167OpenAlexW3022007409MaRDI QIDQ786152

N. M. Gavrikova, Yu. F. Golubev

Publication date: 12 August 2020

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230720010050

zbMATH Keywords

Earth's atmosphereLunar orbitthree-impulse maneuvering schemes

Mathematics Subject Classification ID

Control/observation systems involving computers (process control, etc.) (93C83) Application models in control theory (93C95) Impulsive control/observation systems (93C27)

Uses Software

• DFVLR-SQP

Cites Work

• Formation of high inclined orbits to the ecliptic by multiple gravity assist maneuvers
• Unnamed Item

This page was built for publication: Using a three-impulse maneuvering scheme for returning from the lunar orbit to the reentry point of the Earth's atmosphere