Spacecraft-Trajectory-Design-using-Space-Manifold-Dynamics
Versione 1.0.2 (3,34 MB) da
Arun Suresh
Low Energy trajectories
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
Cita come
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.
Compatibilità della release di MATLAB
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R2021a
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MANIFOLDS
MATLAB MANIFOLDS
PCR3BP/Earth moon/Matlab Code
PCR3BP/Jupiter Europa/Matlab Code
coordinate transformation
dynamic inversion
moon
others
Le versioni che utilizzano il ramo predefinito di GitHub non possono essere scaricate
Versione | Pubblicato | Note della release | |
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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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Per visualizzare o segnalare problemi su questo componente aggiuntivo di GitHub, visita GitHub Repository.