Transfer design methodology between neighborhoods of planetary moons in the circular restricted three-body problem
DC Garcia - 2021 - search.proquest.com
There is an increasing interest in future space missions devoted to the exploration of key
moons in the Solar system. These many different missions may involve libration point orbits …
moons in the Solar system. These many different missions may involve libration point orbits …
A versatile moon-to-moon transfer design method for applications involving libration point orbits
The objective of the present investigation is to present a framework to produce low-energy
trajectories between the vicinities of adjacent moons of a planetary system leveraging …
trajectories between the vicinities of adjacent moons of a planetary system leveraging …
Understanding flow around planetary moons via finite-time Lyapunov exponent maps
D Canales, K Howell - Celestial Mechanics and Dynamical Astronomy, 2024 - Springer
This contribution focuses on the use of finite-time Lyapunov exponent (FTLE) maps to
investigate spacecraft motion within the context of the circular restricted three-body problem …
investigate spacecraft motion within the context of the circular restricted three-body problem …
Immersive Framework for Designing Trajectories Using Augmented Reality
JD Anderson, JA Geliga, KY Tang… - AIAA SCITECH 2024 …, 2024 - arc.aiaa.org
The intuitive interaction capabilities of augmented reality make it ideal for solving complex
3D problems that require complex spatial representations, which is key for astrodynamics …
3D problems that require complex spatial representations, which is key for astrodynamics …
Structure of the NRHO-to-LLO Abort Trajectory Design Space
Starting from Artemis III, the Deep Space Gateway (DSG) will serve as a staging point for the
Human Landing System (HLS), enabling access to multiple regions of the Moon. As the …
Human Landing System (HLS), enabling access to multiple regions of the Moon. As the …