Kea Aerospace

Developed a 6-DOF nonlinear aircraft control system validation suite with configurable test conditions and Monte Carlo testing for a solar-powered stratospheric aircraft, with an image and video of the aircraft shown above. This aircraft, the Atmos, is designed to operate in the stratosphere for extended periods. The validation suite was designed to verify the performance of the aircraft's control system under various flight conditions and to identify potential issues before flight testing.

Due to intellectual property restrictions, I am unable to provide further details about the project.