Piloted simulation study comparing classical and robust flight control design methods

Flight controllers were developed for the F-16 VISTA aircraft using classical PID control design methods in addition to Hinfinity and linear parameter varying (LPV) robust design methods. Desktop analysis and simulation were used to quantitatively assess and compare the performance of each controller. A piloted simulation study was performed to gather qualitative pilot ratings and comments to validate or refute the results and conclusions which were based on the preliminary desktop analysis. Pilot-vehicle describing functions and wavelet analysis techniques were also used to analyze the flight test data gathered during the simulation as a supplement to the quantitative analysis data.