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Standsicherheit
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An Investigation of Rotorcraft Stability-Phase Margin Requirements in Hover
Applications of flight control system methods to an advanced combat rotorcraft
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
Flight-testing and frequency-domain analysis for rotorcraft handling qualities
Flight testing and frequency domain analysis for rotorcraft handling qualities characteristics
Flight-Time Identification of a UH-60A Helicopter and Slung Load
Flying quality analysis and flight evaluation of a highly augmented combat rotorcraft
Formulation and validation of high-order linearized models of helicopter flight mechanics
Frequency-response identification of XV-15 tilt-rotor aircraft dynamics
Helicopter mathematical models and control law development for handling qualities research
High-order state space simulation models of helicopter flight mechanics
Identification of a Full-Envelope Learjet-25 Simulation Model Using a Stitching Architecture
Identification of Linear Time-Periodic Systems from Rotorcraft Flight-Test Data