GitHub - luigigisolfi/Orbital-Mechanics-Exercises: I decided to learn more about Orbital Mechanics, so I started studying and practising. This repository contains commented Python solutions of the exercises taken from the book "Orbital Mechanics for Engineering Students", by H. Curtis.

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I decided to learn more about Orbital Mechanics, so I started studying and practising. This repository contains commented Python solutions of the exercises taken from the book "Orbital Mechanics for Engineering Students", by H. Curtis.

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Name		Name	Last commit message	Last commit date
Latest commit History 1 Commit
Algorithm_3.1_Solve_Kepler_Equation.ipynb		Algorithm_3.1_Solve_Kepler_Equation.ipynb
Algorithm_4.1_From_State_Vector_To_Orbital_Elements.ipynb		Algorithm_4.1_From_State_Vector_To_Orbital_Elements.ipynb
Ex_3.1_ToF_to_Given_True_Anomaly.ipynb		Ex_3.1_ToF_to_Given_True_Anomaly.ipynb
Ex_3.2 .ipynb		Ex_3.2 .ipynb
Ex_3.3.ipynb		Ex_3.3.ipynb
Ex_3.5_Solve_Universal_Kepler_Equation.ipynb		Ex_3.5_Solve_Universal_Kepler_Equation.ipynb
Ex_3.7_Algorithm_3.4_r0_v0_to_find_r_v_at_Dt_later.ipynb		Ex_3.7_Algorithm_3.4_r0_v0_to_find_r_v_at_Dt_later.ipynb
Ex_4.1 Compute Right Ascension and Declination of the ISS given position vector.ipynb		Ex_4.1 Compute Right Ascension and Declination of the ISS given position vector.ipynb
Ex_4.2 Plotting satellite orbit given initial state vector.ipynb		Ex_4.2 Plotting satellite orbit given initial state vector.ipynb
Ex_4.3 From State Vector to Orbital Elements.ipynb		Ex_4.3 From State Vector to Orbital Elements.ipynb