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B. Grebing

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Open access Aug 2026

Design, implementation, and flight testing of a stability augmentation system for coaxial ultralight rotorcraft

This paper describes the first ever flight demonstration of a stability augmentation system using electromechanical inline actuators in a rotorcraft without hydraulic force amplification. A coaxial ultralight helicopter equipped with the stability augmentation system is used as a flight demonstrator. The paper covers...

B. Rothaupt, Walter Fichter, B. Grebing · 0 citations

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