Martin J. Brenner
Actuator and aerodynamic modeling for high-angle-of-attack aeroservoelasticity
Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft
On-line robust modal stability prediction using wavelet processing
Overview of recent flight flutter testing research at NASA Dryden
Wavelet analyses of F/A-18 aeroelastic and aeroservoelastic flight test data