Plot Keplerian / Classical Orbital Elements | Orbital Mechanics with Python 10
Автор: Alfonso Gonzalez - Astrodynamics & SE Podcast
Загружено: 2019-09-02
Просмотров: 2954
Описание:
In this video I go over how to make a plotting function for the keplerian orbital elements over time after orbit propagation. I show how I implemented a 2 rows by 3 columns subplot to include all COEs in one figure. I then implement an example with the ISS orbit and how the keplerian orbital elements change due to the J2 perturbation.
Pre-req videos:
1. Introduction / Overview - • Introduction to Orbital Mechanics with Pyt...
4. Developing the OrbitPropagator Class and the Planetary Data File - • OrbitPropagator Class and Planetary Data F...
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...
8. J2 Perturbation - • J2 Perturbation | Orbital Mechanics with P...
9. rv2coes() Function - • Convert State Vector to Keplerian Orbital ...
Optional videos:
2. Two Body Problem / ODE Solvers - • The Two Body Problem / ODE Solvers | Orbit...
3. Developing the 3D Plotting Function - • Developing the 3D Plotting Function | Orbi...
Link to matplotlib documentation:
https://matplotlib.org/
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