Computational Methods for Feedback Controllers for Aerodynamics Flow Applications

摘要

This report covers the final results of the STTR: 'Computational Methods for Feedback Controllers for Aerodynamics Flow Applications.' It is intended to be a comprehensive summary of the project. The goal of the project was to provide a robust, easy to use computational tool for developing feedback controllers for aerodynamic flow applications - i.e. a tool to develop closed loop flow control methods. The two major partners of the STTR were the USAF Academy's Department of Aeronautics, and Cobalt Solutions, LLC (CSLLC).