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Identification of a Full-Envelope Learjet-25 Simulation Model Using a Stitching Architecture
Identification of Linear Time-Periodic Systems from Rotorcraft Flight-Test Data
Integrating Flight Dynamics & Control Analysis and Simulation in Rotorcraft Conceptual Design
An Investigation of Rotorcraft Stability-Phase Margin Requirements in Hover
Flight Control Development for the ARH-70 Armed Reconnaissance Helicopter Program
Flight Test Identification and Simulation of a UH-60A Helicopter and Slung Load
Flight Control System Development for the BURRO Autonomous UAV
Flight-Time Identification of a UH-60A Helicopter and Slung Load
CONDUIT: A New Multidisciplinary Integration Environment for Flight Control Development