Abstract
This publication shows the semi-empiric noise modeling of an electric-powered vertical takeoff and landing (eVTOL) unmanned aerial vehicle (UAV) by means of system identification from flight noise measurement data. This work aims to provide noise models with a compact analytical ansatz for horizontal and vertical flight which are suited for integration into a geographical information system. Therefore, flight noise measurement campaigns were conducted and evaluated. An existing noise model ansatz is adapted to the eVTOL UAV under consideration and noise models are computed from the measurement data using the output error method. The resulting models are checked for plausibility by comparing them to technical literature. The horizontal flight noise model is subjected to a correlation analysis and the influence of meteorological effects are examined. To achieve a higher level of accuracy in future noise modelings, an optimization of the microphone positions as well as the flight trajectory is carried out.
Original language | English |
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Pages (from-to) | 85-96 |
Number of pages | 12 |
Journal | CEAS Aeronautical Journal |
Volume | 13 |
Issue number | 1 |
DOIs | |
State | Published - Jan 2022 |
Keywords
- Flight noise measurement
- Noise modeling
- Output error method
- UAV
- Urban air mobility
- eVTOL