Controlled short-period orbits around Earth-Moon equilateral libration points for Lunar Occultations
This paper proposes a framework for a satellite mission with the goal to perform Lunar
Occultations within the context of the circular restricted three-body problem (CR3BP) of the …
Occultations within the context of the circular restricted three-body problem (CR3BP) of the …
Utilizing the geometric mechanics framework to predict attitude in a full ephemeris model of the Cislunar region
Predicting the attitude of spacecraft traveling within the Cislunar region is crucial to ensure
the success of future missions planned within that realm of space. To consider the coupled …
the success of future missions planned within that realm of space. To consider the coupled …
Mission concept and transfer analysis for a CisLunar environment CubeSat mission
M Casanovas Crespo - 2024 - upcommons.upc.edu
This master's thesis presents an in-depth analysis of the mission concept and transfer
trajectory design for a small probe, with the size of a 12U CubeSat, operating in the Cislunar …
trajectory design for a small probe, with the size of a 12U CubeSat, operating in the Cislunar …
Feedback Control Methods on Short-Period Orbits Of the Earth-Moon Equilateral Libration Points
LE Mendoza Zambrano, F Criscola, D Canales Garcia… - 2023 - commons.erau.edu
Recent research by the authors suggests a unique approach to perform Lunar occultations
for a diverse set of scientific applications. Under the circular restricted three-body problem …
for a diverse set of scientific applications. Under the circular restricted three-body problem …
[PDF][PDF] FEEDBACK CONTROL METHODS ON SHORT-PERIOD ORBITS OF THE EARTH-MOON EQUILATERAL LIBRATION POINTS
LEM Zambrano, F Criscola, D Canales, R Bevilacqua… - researchgate.net
Recent research by the authors suggests a unique approach to perform Lunar occultations
for a diverse set of scientific applications. Under the circular restricted three-body problem …
for a diverse set of scientific applications. Under the circular restricted three-body problem …