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.
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.
Python coded tool for wing structural sizing. Given the wing shape, material constraints and aerodynamical loading, all the necessary structural elements are shaped and placed to be compliant with safety regulations.