N-body Perturbations Software | Orbital Mechanics with Python 18

Описание: In this video I go over how to implement the n-body perturbation into the differential equation of OrbitPropagator. I cover a few examples of how the gravitational pull of the moon affects different types of orbits. I also mentioned the irregularities of the lunar orbit.

Pre-req videos:
1. Introduction / Overview -    • Introduction to Orbital Mechanics with Pyt...  
2. Two Body Problem / ODE Solvers -    • The Two Body Problem / ODE Solvers | Orbit...  
4. Developing the OrbitPropagator Class and the Planetary Data File -    • OrbitPropagator Class and Planetary Data F...  
8. J2 Perturbation -    • J2 Perturbation | Orbital Mechanics with P...  
17. N-body Perturbation Theory -    • N-body Perturbation Theory | Orbital Mecha...  

Optional videos:
3. Developing the 3D Plotting Function -    • Developing the 3D Plotting Function | Orbi...  
5. tools.py and the plot_n_orbits() function -    • Tools file and the plot_n_orbits() Functio...  
6. Keplerian Orbital Elements -    • Keplerian / Classical Orbital Elements | O...  
9. rv2coes() Function -    • Convert State Vector to Keplerian Orbital ...  
10. Plotting the Keplerian / Classical Orbital Elements -    • Plot Keplerian / Classical Orbital Element...  

Link to spiceypy documentation:
https://spiceypy.readthedocs.io/en/ma...