2023
DOI: 10.1016/j.pss.2023.105684
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The sounds of a helicopter on Mars

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Cited by 6 publications
(10 citation statements)
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“…After showing the attenuation coefficient and the speed of sound for a wide range of frequencies in Section 3.2 we focus on a few frequencies, namely 10, 100, 1,000, and 10,000 Hz, in order to demonstrate the frequency dependence of certain effects. When it is not convenient to show too many frequencies, we focus on 100 Hz as it is representative of the sound produced by Ingenuity, the helicopter traveling along Perseverance rover (R. D. Lorenz et al., 2023), which produces sound at its blade passage frequency (84 Hz) and at its first harmonic (168 Hz). Similarly, after showing the attenuation coefficient and the speed of sound at every point of the Martian surface in Section 3.4 we have chosen to focus on a few locations and especially Perseverance site.…”
Section: Resultsmentioning
confidence: 99%
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“…After showing the attenuation coefficient and the speed of sound for a wide range of frequencies in Section 3.2 we focus on a few frequencies, namely 10, 100, 1,000, and 10,000 Hz, in order to demonstrate the frequency dependence of certain effects. When it is not convenient to show too many frequencies, we focus on 100 Hz as it is representative of the sound produced by Ingenuity, the helicopter traveling along Perseverance rover (R. D. Lorenz et al., 2023), which produces sound at its blade passage frequency (84 Hz) and at its first harmonic (168 Hz). Similarly, after showing the attenuation coefficient and the speed of sound at every point of the Martian surface in Section 3.4 we have chosen to focus on a few locations and especially Perseverance site.…”
Section: Resultsmentioning
confidence: 99%
“…Measurements of speed of sound (Maurice et al, 2022) and attenuation coefficient (Chide et al, 2023) have been published at different frequencies using the helicopter and the LIBS instrument. The helicopter produces sound at its blade passage frequency, 84 Hz, and its first harmonic 168 Hz (R. D. Lorenz et al, 2023) whereas LIBS sounds ranges from 3 to 21 kHz (Chide et al, 2023). The helicopter flies at an altitude of 5-10 m above the ground, the microphone is 1.8 m from the ground and the LIBS experiment shockwaves are located on the ground.…”
Section: In Situ Experimental Validationmentioning
confidence: 99%
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“…Since results will be discussed in terms of transmission loss or excess attenuation, the amplitude of the source can be fixed arbitrarily. In the following, the source level is of 100 dB at 10 cm from the point source, which can be understood as the approximate order of magnitude of a UAV rotor noise on Mars (Lorenz et al, 2023). The sound equation in the far field (r ≫ 1 0 , k 1 0 around 40 cm for a 100 Hz wave near the Martian surface) becomes the two-dimensional Helmholtz differential equation when the axisymmetric assumption is applied…”
Section: The Parabolic Equation (Pe) Methodsmentioning
confidence: 99%
“…Given the harsh flight conditions on Mars, as well as the significant time delays in communication between Mars and Earth, coupled with the absence of GPS navigation, there exists an urgent imperative to address the technological challenges associated with the control of rotary-wing Mars UAVs and their compatibility with the Martian flight environment [96,97]. Furthermore, due to the spatial constraints of rotary-wing Mars UAVs, it is often necessary to employ control strategies specifically tailored to coaxial rotary-wing Mars UAVs.…”
Section: Research On Control Methods Of Rotary-wing Mars Uavsmentioning
confidence: 99%