An approach to minimize aircraft motion bias in multi-hole probe wind measurements made by small unmanned aerial systems

<p>A multi-hole probe mounted on an aircraft provides the air velocity vector relative to the aircraft, requiring knowledge of the aircraft spatial orientation (e.g., Euler angles), translational velocity and angular velocity to translate this information to an Earth-based reference frame an...

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Main Authors: L. Al-Ghussain, S. C. C. Bailey
Format: Article
Language:English
Published: Copernicus Publications 2021-01-01
Series:Atmospheric Measurement Techniques
Online Access:https://amt.copernicus.org/articles/14/173/2021/amt-14-173-2021.pdf
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spelling doaj-b7b6b2f104f94d34b50b09d30a6f39f02021-01-11T14:28:24ZengCopernicus PublicationsAtmospheric Measurement Techniques1867-13811867-85482021-01-011417318410.5194/amt-14-173-2021An approach to minimize aircraft motion bias in multi-hole probe wind measurements made by small unmanned aerial systemsL. Al-GhussainS. C. C. Bailey<p>A multi-hole probe mounted on an aircraft provides the air velocity vector relative to the aircraft, requiring knowledge of the aircraft spatial orientation (e.g., Euler angles), translational velocity and angular velocity to translate this information to an Earth-based reference frame and determine the wind vector. As the relative velocity of the aircraft is typically an order of magnitude higher than the wind velocity, the extracted wind velocity is very sensitive to multiple sources of error including misalignment of the probe and aircraft coordinate system axes, sensor error and misalignment in time of the probe and aircraft orientation measurements in addition to aerodynamic distortion of the velocity field by the aircraft. Here, we present an approach which can be applied after a flight to identify and correct biases which may be introduced into the final wind measurement. The approach was validated using a ground reference, different aircraft and the same aircraft at different times. The results indicate a significant reduction in wind velocity variance at frequencies which correspond to aircraft motion.</p>https://amt.copernicus.org/articles/14/173/2021/amt-14-173-2021.pdf
collection DOAJ
language English
format Article
sources DOAJ
author L. Al-Ghussain
S. C. C. Bailey
spellingShingle L. Al-Ghussain
S. C. C. Bailey
An approach to minimize aircraft motion bias in multi-hole probe wind measurements made by small unmanned aerial systems
Atmospheric Measurement Techniques
author_facet L. Al-Ghussain
S. C. C. Bailey
author_sort L. Al-Ghussain
title An approach to minimize aircraft motion bias in multi-hole probe wind measurements made by small unmanned aerial systems
title_short An approach to minimize aircraft motion bias in multi-hole probe wind measurements made by small unmanned aerial systems
title_full An approach to minimize aircraft motion bias in multi-hole probe wind measurements made by small unmanned aerial systems
title_fullStr An approach to minimize aircraft motion bias in multi-hole probe wind measurements made by small unmanned aerial systems
title_full_unstemmed An approach to minimize aircraft motion bias in multi-hole probe wind measurements made by small unmanned aerial systems
title_sort approach to minimize aircraft motion bias in multi-hole probe wind measurements made by small unmanned aerial systems
publisher Copernicus Publications
series Atmospheric Measurement Techniques
issn 1867-1381
1867-8548
publishDate 2021-01-01
description <p>A multi-hole probe mounted on an aircraft provides the air velocity vector relative to the aircraft, requiring knowledge of the aircraft spatial orientation (e.g., Euler angles), translational velocity and angular velocity to translate this information to an Earth-based reference frame and determine the wind vector. As the relative velocity of the aircraft is typically an order of magnitude higher than the wind velocity, the extracted wind velocity is very sensitive to multiple sources of error including misalignment of the probe and aircraft coordinate system axes, sensor error and misalignment in time of the probe and aircraft orientation measurements in addition to aerodynamic distortion of the velocity field by the aircraft. Here, we present an approach which can be applied after a flight to identify and correct biases which may be introduced into the final wind measurement. The approach was validated using a ground reference, different aircraft and the same aircraft at different times. The results indicate a significant reduction in wind velocity variance at frequencies which correspond to aircraft motion.</p>
url https://amt.copernicus.org/articles/14/173/2021/amt-14-173-2021.pdf
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