Flight Test Identification and Simulation of a UH-60A Helicopter and Slung Load
CONDUIT: A New Multidisciplinary Integration Environment for Flight Control Development
System identification methods for aircraft flight control development and validation
Digital control of highly augmented combat rotorcraft
Demonstration of frequency-sweep testing technique using a Bell 214-ST helicopter
Flight-Time Identification of a UH-60A Helicopter and Slung Load
Applications of flight control system methods to an advanced combat rotorcraft
Frequency-response identification of XV-15 tilt-rotor aircraft dynamics