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Stabilität
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keywords:(Stabilität)
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
Integrating Flight Dynamics & Control Analysis and Simulation in Rotorcraft Conceptual Design
Piloting considerations for terminal area operations of civil tiltwing and tiltrotor aircraft
System identification methods for aircraft flight control development and validation
System identification requirements for high-bandwidth rotorcraft flight control system design
System identification requirements for high-bandwidth rotorcraft flight control system design