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

version 1.0.0 (450 KB) by Arun Suresh
Low Energy trajectories

19 Downloads

Updated 13 Apr 2021

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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

Arun Suresh (2021). Spacecraft-Trajectory-Design-using-Space-Manifold-Dynamics (https://github.com/arunsuresh990/Spacecraft-Trajectory-Design-using-Space-Manifold-Dynamics), GitHub. Retrieved .

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

MATLAB MANIFOLDS

PCR3BP/Earth moon/Matlab Code

PCR3BP/Jupiter Europa/Matlab Code

coordinate transformation

dynamic inversion

moon

others

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.