Assessing Head Injury of Civilian UAV Safety Systems: A Test Apparatus and Spherical Shell Example

In recent years, flying vehicles have become an innovative way to transfer parcels efficiently over a short distance. Existing airspace regulations are slow to adapt to the anticipated rise in aircraft traffic resulting from this development. This is because the increase in unmanned aerial vehicles...

Full description

Saved in:
Bibliographic Details
Main Authors: Eric J. Hettel, Hossein Eslamiat, Mohammed Aleemuddin, Mohsen Farajijalal
Format: Article
Language:English
Published: IEEE 2025-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/11104057/
Tags: Add Tag
No Tags, Be the first to tag this record!
_version_ 1849393812891238400
author Eric J. Hettel
Hossein Eslamiat
Mohammed Aleemuddin
Mohsen Farajijalal
author_facet Eric J. Hettel
Hossein Eslamiat
Mohammed Aleemuddin
Mohsen Farajijalal
author_sort Eric J. Hettel
collection DOAJ
description In recent years, flying vehicles have become an innovative way to transfer parcels efficiently over a short distance. Existing airspace regulations are slow to adapt to the anticipated rise in aircraft traffic resulting from this development. This is because the increase in unmanned aerial vehicles (UAVs) comes with an increased risk of personal injuries from faulty drones carrying a payload. Many national regulatory agencies, such as the FAA, rely on the Abbreviated Injury Scale (AIS) to determine the weight threshold of a UAV by evaluating the impact energy and correlating it to the severity of a potential injury. This research paper presents a test apparatus to investigate the effect of different safety systems on AIS.As an example, a passive safety system in the form of a geodesic shell is used to investigate the change in impact acceleration and therefore, the head injury sustained. The spherical shell is designed as a geodesic sphere. Its struts are carbon fiber reinforced polymer (CFRP) rods and connectors made from a flexible filament, TPU-95A. The apparatus enables droppings of the geodesic shell from a height of 4.48 meters,varying the payload weight in two weight classes between 2.5 lb to 5 lb attached to the drone. The impact acceleration is recorded, and the impact velocity is calculated using slow-motion video. The Head Injury Criterion (HIC) scale and the Abbreviated Injury Scale (AIS) are used to measure the predicted head injury level. The test apparatus designed establishes a standard of testing for other safety systems, in addition to geodesic shells like airbags, to be tested for their efficacy in reducing the head injury level sustained.
format Article
id doaj-art-dfe1f304b4244441847e4193ed63c45f
institution Kabale University
issn 2169-3536
language English
publishDate 2025-01-01
publisher IEEE
record_format Article
series IEEE Access
spelling doaj-art-dfe1f304b4244441847e4193ed63c45f2025-08-20T03:40:17ZengIEEEIEEE Access2169-35362025-01-011313659813661110.1109/ACCESS.2025.359393711104057Assessing Head Injury of Civilian UAV Safety Systems: A Test Apparatus and Spherical Shell ExampleEric J. Hettel0Hossein Eslamiat1https://orcid.org/0000-0001-6043-1505Mohammed Aleemuddin2https://orcid.org/0009-0002-3208-8994Mohsen Farajijalal3https://orcid.org/0009-0008-8389-7138School of Mechanical, Aerospace, and Materials Engineering, Southern Illinois University, Carbondale, IL, USASchool of Mechanical, Aerospace, and Materials Engineering, Southern Illinois University, Carbondale, IL, USASchool of Mechanical, Aerospace, and Materials Engineering, Southern Illinois University, Carbondale, IL, USADepartment of Mechanical Engineering, University of California at Merced, Merced, CA, USAIn recent years, flying vehicles have become an innovative way to transfer parcels efficiently over a short distance. Existing airspace regulations are slow to adapt to the anticipated rise in aircraft traffic resulting from this development. This is because the increase in unmanned aerial vehicles (UAVs) comes with an increased risk of personal injuries from faulty drones carrying a payload. Many national regulatory agencies, such as the FAA, rely on the Abbreviated Injury Scale (AIS) to determine the weight threshold of a UAV by evaluating the impact energy and correlating it to the severity of a potential injury. This research paper presents a test apparatus to investigate the effect of different safety systems on AIS.As an example, a passive safety system in the form of a geodesic shell is used to investigate the change in impact acceleration and therefore, the head injury sustained. The spherical shell is designed as a geodesic sphere. Its struts are carbon fiber reinforced polymer (CFRP) rods and connectors made from a flexible filament, TPU-95A. The apparatus enables droppings of the geodesic shell from a height of 4.48 meters,varying the payload weight in two weight classes between 2.5 lb to 5 lb attached to the drone. The impact acceleration is recorded, and the impact velocity is calculated using slow-motion video. The Head Injury Criterion (HIC) scale and the Abbreviated Injury Scale (AIS) are used to measure the predicted head injury level. The test apparatus designed establishes a standard of testing for other safety systems, in addition to geodesic shells like airbags, to be tested for their efficacy in reducing the head injury level sustained.https://ieeexplore.ieee.org/document/11104057/Aerospace safetycollision tolerancedronesinjuriesspherical shellUAV crash testing
spellingShingle Eric J. Hettel
Hossein Eslamiat
Mohammed Aleemuddin
Mohsen Farajijalal
Assessing Head Injury of Civilian UAV Safety Systems: A Test Apparatus and Spherical Shell Example
IEEE Access
Aerospace safety
collision tolerance
drones
injuries
spherical shell
UAV crash testing
title Assessing Head Injury of Civilian UAV Safety Systems: A Test Apparatus and Spherical Shell Example
title_full Assessing Head Injury of Civilian UAV Safety Systems: A Test Apparatus and Spherical Shell Example
title_fullStr Assessing Head Injury of Civilian UAV Safety Systems: A Test Apparatus and Spherical Shell Example
title_full_unstemmed Assessing Head Injury of Civilian UAV Safety Systems: A Test Apparatus and Spherical Shell Example
title_short Assessing Head Injury of Civilian UAV Safety Systems: A Test Apparatus and Spherical Shell Example
title_sort assessing head injury of civilian uav safety systems a test apparatus and spherical shell example
topic Aerospace safety
collision tolerance
drones
injuries
spherical shell
UAV crash testing
url https://ieeexplore.ieee.org/document/11104057/
work_keys_str_mv AT ericjhettel assessingheadinjuryofcivilianuavsafetysystemsatestapparatusandsphericalshellexample
AT hosseineslamiat assessingheadinjuryofcivilianuavsafetysystemsatestapparatusandsphericalshellexample
AT mohammedaleemuddin assessingheadinjuryofcivilianuavsafetysystemsatestapparatusandsphericalshellexample
AT mohsenfarajijalal assessingheadinjuryofcivilianuavsafetysystemsatestapparatusandsphericalshellexample