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System identification requirements for high-bandwidth rotorcraft flight control system design
System identification requirements for high-bandwidth rotorcraft flight control system design
System identification methods for aircraft flight control development and validation
Integrating Flight Dynamics & Control Analysis and Simulation in Rotorcraft Conceptual Design
Identification of Linear Time-Periodic Systems from Rotorcraft Flight-Test Data
Identification of a Full-Envelope Learjet-25 Simulation Model Using a Stitching Architecture
High-order state space simulation models of helicopter flight mechanics
Helicopter mathematical models and control law development for handling qualities research
Frequency-response identification of XV-15 tilt-rotor aircraft dynamics
Formulation and validation of high-order linearized models of helicopter flight mechanics
Flying quality analysis and flight evaluation of a highly augmented combat rotorcraft
Flight-Time Identification of a UH-60A Helicopter and Slung Load
Flight testing and frequency domain analysis for rotorcraft handling qualities characteristics
Flight-testing and frequency-domain analysis for rotorcraft handling qualities
Flight Test Identification and Simulation of a UH-60A Helicopter and Slung Load
Flight Control System Development for the BURRO Autonomous UAV
Flight Control Development for the ARH-70 Armed Reconnaissance Helicopter Program
Digital control of highly augmented combat rotorcraft
Demonstration of frequency-sweep testing technique using a Bell 214-ST helicopter
CONDUIT: A New Multidisciplinary Integration Environment for Flight Control Development
Applications of flight control system methods to an advanced combat rotorcraft
An Investigation of Rotorcraft Stability-Phase Margin Requirements in Hover