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 project outputs G-code that is used to control a 4-axis hot wire cutter, employed to cut a wing / airfoil from a physical block of foam. Effectively, it is a slicer for a particular arrangement of raw-coordinate data files.
A Transformation Script for converting from the WINGS Framework to OPMW and PROV frameworks. The Transformation Script utilizes the Jena Framework in Java. Multiple aspects of the WINGS Workflow System are captured in the script including the Expanded Template. Further, it includes several tests for its validity and consistency.