Near-Rectilinear Halo Orbit Analysis for the Artemis Lunar Gateway Mission

Technical analysis of NRHO trajectories for NASA's Artemis Lunar Gateway station using NASA GMAT. Demonstrates orbital characteristics, stability analysis, and mission design for cislunar infrastructure.

Authors

Ginevra Cianci

Institutions

Politecnico di Torino (IT)
Turin Polytechnic University (UZ)

Publication Details

Journal: Zenodo (CERN European Organization for Nuclear Research)
Published: 2026-02-02
DOI: https://doi.org/10.5281/zenodo.18454887
Primary Topic: Spacecraft Dynamics and Control
Type: article
Field-Weighted Citation Impact: 0.00

Controls

|||

ALL TIME

JAN

FEB

MAR

APR

MAY

JUN

JUL

AUG

SEP

OCT

article

Near-Rectilinear Halo Orbit Analysis for the Artemis Lunar Gateway Mission

Ginevra Cianci

Feb 2, 2026

Zenodo (CERN European Organization for Nuclear Research)

Spacecraft Dynamics and Control

article

Near-Rectilinear Halo Orbit Analysis for the Artemis Lunar Gateway Mission

Ginevra Cianci

February 2, 2026article en

Abstract

Zenodo (CERN European Organization for Nuclear Research)

Politecnico di Torino (IT), Turin Polytechnic University (UZ)

Industry, innovation and infrastructure

Openalex Percentile: Top 70%

Spacecraft Dynamics and Control

DOI Open Access PDF OpenAlex

AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.

Near-Rectilinear Halo Orbit Analysis for the Artemis Lunar Gateway Mission — Ginevra Cianci · Zenodo (CERN European Organization for Nuclear Research) (2026) | TGRS Research Map | TGRS