Spacecraft atmospheric entry simulations using Python
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Updated
Nov 27, 2020 - Python
Spacecraft atmospheric entry simulations using Python
ParaView template project for orbital data visualization (orbits, trajectory points, ground station field of view)
A quick-and-dirty SQL database for storing the historical orbital elements of satellites, including a script for trawling data from Celestrak and Space Track to populate the database.
Capstone project for Spacecraft Dynamics and Control course
An entry into to the world of spacecraft trajectory design and optimization. The problem statement is to capture two planetary systems with one launch from earth, which means the initial part of the trajectory of a spacecraft which separates into two has to be the same. After separation, one half of the spacecraft will capture Saturn after takin…
A tool for planning flights from one celestial body in KSP to another
My quest to learn JAX and make an autograd implementation of the Q-Law
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