Utilizing the geometric mechanics framework to predict attitude in a full ephemeris model of the Cislunar region
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Publication:6183820
DOI10.1016/J.CNSNS.2023.107726OpenAlexW4388968372MaRDI QIDQ6183820
Morad Nazari, Brennan McCann, Annika Anderson, David Canales
Publication date: 23 January 2024
Published in: Communications in Nonlinear Science and Numerical Simulation (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.cnsns.2023.107726
perturbation methodrotational motiontranslational motionLyapunov orbitspacecraft attitudecircular restricted full three-body problemLunar transferretrograde orbit
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