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Airspeed estimation for UAVs using only propeller feedback
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DOI：10.1016/j.ast.2025.110999.png)
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Abstract
En 中文
• Airspeed estimation using propeller power and rotational speed measurements. • Analytical airspeed model derived from simulation and experimental data. • Estimates airspeed without requiring a dynamic model of the vehicle. • In-flight identification of the model coefficients enables autonomous deployment. • Airspeed prediction error 5% in nominal forward flight conditions.
Keywords:
UAV airspeed estimation
airspeed analytical redundancy
propeller feedback
in-flight identification
data-driven modeling
BEM
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