You signed in with another tab or window. Reload to refresh your session.You signed out in another tab or window. Reload to refresh your session.You switched accounts on another tab or window. Reload to refresh your session.Dismiss alert
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.
This projects aims to use matrix calculus to determine the forces and displacements of the structures thus to obtain the stress state of each member of the bar, either traction (+) or compression (-).
This MATLAB live code tool can morph any given airfoil file with user-defined flap and slat settings. There are two types of flaps and slats that can be generated - Hinged and Continuous
This project aims to study the dynamic behavior of a simplified model of an aircraft when rolling (steady state) when it is circulating stationary on the runway. The roughness of the track is the main exciting agent that will be considered in this project.