Spacecraft-Trajectory-Design-using-Space-Manifold-Dynamics
Low Energy trajectories
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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
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.
General Information
- Version 1.0.2 (3.34 MB)
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View License on GitHub
MATLAB Release Compatibility
- Compatible with any release
Platform Compatibility
- Windows
- macOS
- Linux
Versions that use the GitHub default branch cannot be downloaded
| Version | Published | Release Notes | Action |
|---|---|---|---|
| 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 |
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| 1.0.1 | Modified Link |
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| 1.0.0 |
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To view or report issues in this GitHub add-on, visit the GitHub Repository.
