What is it about?
Helicopter roll may force the pilot to unintentionally move the control stick in a manner that further excites the roll motion. We numerically simulated and verified this in the flight simulator.
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Why is it important?
The phenomenon was studied, simulated, and experimentally reproduced in the flight simulator using accurate numerical models and skilled test pilots. Some helicopters may be particularly susceptible to the problem. In the future, the spread of flight control systems and automation may cause its insurgence, unless its possibility is detected and prevented by design.
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Read the Original
This page is a summary of: Prediction and Simulator Verification of Roll/Lateral Adverse Aeroservoelastic Rotorcraft–Pilot Couplings, Journal of Guidance Control and Dynamics, January 2016, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g001121.
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Resources
Robust Stability Analysis of Adverse Aeroelastic Roll/Lateral Rotorcraft-Pilot Couplings
Paper that proposes a simple model for a parametric study of the problem V. Muscarello, P. Masarati, G. Quaranta, "Robust Stability Analysis of Adverse Aeroelastic Roll/Lateral Rotorcraft-Pilot Couplings", J. of the American Helicopter Society, 62(2):1-13, April 2017, doi:10.4050/JAHS.62.022003.
Instability Mechanism of Roll/Lateral Biodynamic Rotorcraft-Pilot Couplings
Paper that compares different analysis techniques suitable for highlighting the problem V. Muscarello, P. Masarati, G. Quaranta, G. Tod, J. Gomand, F. Malburet, M. D. Pavel, "Instability Mechanism of Roll/Lateral Biodynamic Rotorcraft-Pilot Couplings", J. of the American Helicopter Society, 63(2):1-13, April 2018, doi:10.4050/JAHS.63.022004.
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