Spacecraft-Trajectory-Design-using-Space-Manifold-Dynamics

Version 1.0.2 (3.34 MB) by Arun Suresh
Low Energy trajectories
3.0
(1)
96 Downloads
Updated 26 Feb 2023
View License on GitHub
Low Energy trajectories that mostly utilises natural dynamics are now used to design successful and efficient missions. A single spacecraft is designed to orbit moons of Jupiter, Ganymede and Europa. The mission utilizes dynamical channels in the phase space which connects the vicinity of Ganymede to that of Europa. The system is highly nonlinear and dependent on initial condition. Dynamic equations are obtained and a controller based on the dynamic inverse is synthesized for the purpose of stabilization and trajectory tracking

Cite As

A Suresh, UP Rajeev, WC ArunKishore, "Heteroclinic Connection in Galilean Moon Orbiter Mission Using Space Manifold Dynamics," National Conference on Technological Trends, Trivandrum, Kerala, India, 2015.

MATLAB Release Compatibility
Created with R2021a
Compatible with any release
Platform Compatibility
Windows macOS Linux
Tags Add Tags

Community Treasure Hunt

Find the treasures in MATLAB Central and discover how the community can help you!

Start Hunting!

MANIFOLDS

MATLAB MANIFOLDS

PCR3BP/Earth moon/Matlab Code

PCR3BP/Jupiter Europa/Matlab Code

coordinate transformation

dynamic inversion

moon

others

Versions that use the GitHub default branch cannot be downloaded

Version Published Release Notes
1.0.2

See release notes for this release on GitHub: https://github.com/arunsuresh990/Spacecraft-Trajectory-Design-using-Space-Manifold-Dynamics/releases/tag/V1.0.2
1.0.1

Modified Link
1.0.0

To view or report issues in this GitHub add-on, visit the GitHub Repository.
To view or report issues in this GitHub add-on, visit the GitHub Repository.