Design of a Multiple Input-Multiple Output Flight Control System Containing Uncertain Parameters
Multivariable Digital Control Laws for the UH-60A Black Hawk Helicopter
Evaluation of a Digital Flight Controller for a Flexible-Fighter Aircraft
New Flutter Analysis Technique for Time-Domain Computational Aeroelasticity
Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
Rotorcraft Flight Control Design Using Quantitative Feedback Theory and Dynamic Crossfeeds
Analysis of Computational Aeroelastic Simulations by Fitting Time Signals
Identification of SA-330 PUMA Dynamic Models from Flight Test Data in Frequency Domain