earth_moon_orbit_animation
Note: must also be used with earth_moon_orbit_ode45 at https://www.mathworks.com/matlabcentral/fileexchange/71313-earth_moon_orbit_ode45
Depicts the path in 3 dimensions of a projectile being affected by the gravity of the Earth and the Moon using both the Classical 4th Order Runge-Kutta Method and Euler's Method. A special thank you to Professor Mark Edelen who taught the Mat-lab Programming & Numerical Methods class at Howard Community College. He created a program similar to this that simulated Apollo 13's flight path which inspired this program, and believed in my ability to create such a program.
See also https://www.mathworks.com/matlabcentral/fileexchange/69476-earth_moon_orbit_va-riable_timesteps for a similar version of this program
Citation pour cette source
Aryeh Laks (2024). earth_moon_orbit_animation (https://www.mathworks.com/matlabcentral/fileexchange/70598-earth_moon_orbit_animation), MATLAB Central File Exchange. Récupéré le .
Compatibilité avec les versions de MATLAB
Plateformes compatibles
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- Sciences > Earth, Ocean, and Atmospheric Sciences > Earth and Planetary Science >
- Engineering > Aerospace Engineering > Satellite and Orbital Mechanics >
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Version | Publié le | Notes de version | |
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1.0.1 | Math error was found and corrected. ode45 was added in to check the results of the other methods. Graphics were updated. |
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1.0.0 |