An Investigation of Rotorcraft Stability-Phase Margin Requirements in Hover
Applications of flight control system methods to an advanced combat rotorcraft
Business Jet Fly-by-Wire Control Laws Handling Qualities Flight Test Assessment
CONDUIT: A New Multidisciplinary Integration Environment for Flight Control Development
Demonstration of frequency-sweep testing technique using a Bell 214-ST helicopter
Digital control of highly augmented combat rotorcraft
Flight Control Development for the ARH-70 Armed Reconnaissance Helicopter Program
Flight Control System Development for the BURRO Autonomous UAV
Flight Test Identification and Simulation of a UH-60A Helicopter and Slung Load