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Stabilität
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keywords:(Stabilität)
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
System identification methods for aircraft flight control development and validation
Flight testing and frequency domain analysis for rotorcraft handling qualities characteristics
System identification requirements for high-bandwidth rotorcraft flight control system design
Formulation and validation of high-order linearized models of helicopter flight mechanics
Applications of flight control system methods to an advanced combat rotorcraft
Helicopter mathematical models and control law development for handling qualities research
Demonstration of frequency-sweep testing technique using a Bell 214-ST helicopter
Frequency-response identification of XV-15 tilt-rotor aircraft dynamics
Digital control of highly augmented combat rotorcraft