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This is a MATLAB project made for the Flight Dynamics course in the aerospace undergraduate program that allows to make an stability analysis for a Cessna 310 aircraft in approach condition.
"This is a work in progress where an engineering analysis is conducted on the testing system for the rockets of the Uniandino Aerospace Project (PUA), using the Arcadia method and the open-source s…
This code was developed as the first project for the astrophysics course in the aerospace engineering undergraduate program. It utilizes the astroquery library from JPL to extract astrodynamics dat…
This code was created as an assignment for the planetary astrophysics course with the goal of building an independent solar system to analyze the dynamic stability of planets over time using the Me…