Flight Control Development for the ARH-70 Armed Reconnaissance Helicopter Program
An Investigation of Rotorcraft Stability-Phase Margin Requirements in Hover
Integrating Flight Dynamics & Control Analysis and Simulation in Rotorcraft Conceptual Design
Flight Test Identification and Simulation of a UH-60A Helicopter and Slung Load
Flight Control System Development for the BURRO Autonomous UAV
CONDUIT: A New Multidisciplinary Integration Environment for Flight Control Development
Demonstration of frequency-sweep testing technique using a Bell 214-ST helicopter
Flight-testing and frequency-domain analysis for rotorcraft handling qualities
Flight testing and frequency domain analysis for rotorcraft handling qualities characteristics