Correction: Psychoacoustic Characterization of Multirotor Drones in Realistic Flyover Maneuvers

Conference paper (2024)

Authors

R.M. Yupa Villanueva Aircraft Noise and Climate Effects - Aerospace Engineering
R. Merino Martinez Aircraft Noise and Climate Effects - Aerospace Engineering
A. Altena Aircraft Noise and Climate Effects - Aerospace Engineering
M. Snellen Control & Operations
Research Group
Aircraft Noise and Climate Effects (Aerospace Engineering) (TU Delft)
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Published Date

2024

Language

English

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Faculty

Aerospace Engineering

Department

Control & Operations

Research Group

Aircraft Noise and Climate Effects

Abstract

Correction Notice • Place s5 in front of the symbols ‘greater than or equal to (≥)’ and ‘less than (<)’ in Equation 2, as shown below. (Formula Presented). • Replace the correlation coefficient ‘0.886’ showed in Table 6 to ‘-0.886’. This correction also apply to the paragraph below Section 3 (Correlation between Annoyance and Drone Characteristics) and in the last paragraph of the Conclusions. This negative value indicates an inverse relationship between the installation ratio (d/D) and the annoyance computed using the More PA model. • Replace ‘0.337 (Zwicker PA model)’ by ‘0.362 (Willemsen PA model)’ in the paragraph below Section 3 (Correlation between Annoyance and Drone Characteristics). This value (0.362) is also reported in Table 6.

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