Matlab implementation to simulate the non-linear dynamics of a fixed-wing unmanned areal glider. Includes tools to calculate aerodynamic coefficients using a vortex lattice method implementation, and to extract longitudinal and lateral linear systems around the trimmed gliding state.

PteraControls is a tool for designing control systems for flapping wing vehicles.

This paper graphically presents the evolutions of several variables during the re-entry of two types of vehicles: Ballistic and Supporters

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.

Repo for some modelling and simulation work relating to my thesis