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Regelbarkeit
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Integrating Flight Dynamics & Control Analysis and Simulation in Rotorcraft Conceptual Design
Flight Control System Development for the BURRO Autonomous UAV
Flight-Time Identification of a UH-60A Helicopter and Slung Load
Flight Testing and Frequency Domain Analysis for Rotorcraft Handling Qualities Characteristics
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