Collision severity evaluation of quadcopter UAV crash on human head

This study focuses on determining the collision severity of a generalised quadcopter Unmanned Aerial Vehicle (UAV) crash on the human head. Finite Element Analysis (FEA) and explicit dynamics simulations on ABAQUS were used to determine the peak impact force. In this study, appropriate dimensions fo...

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Main Author: Suresh S/O Ravi
Other Authors: Low Kin Huat
Format: Final Year Project
Language:English
Published: Nanyang Technological University 2023
Subjects:
Online Access:https://hdl.handle.net/10356/167408
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1674082023-05-27T16:51:38Z Collision severity evaluation of quadcopter UAV crash on human head Suresh S/O Ravi Low Kin Huat School of Mechanical and Aerospace Engineering MKHLOW@ntu.edu.sg Engineering::Aeronautical engineering::Aircraft Engineering::Mathematics and analysis::Simulations This study focuses on determining the collision severity of a generalised quadcopter Unmanned Aerial Vehicle (UAV) crash on the human head. Finite Element Analysis (FEA) and explicit dynamics simulations on ABAQUS were used to determine the peak impact force. In this study, appropriate dimensions for the modelling of a generalised quadcopter UAV were obtained from dimensional analysis on Civil Aviation Authority of Singapore (CAAS) 2022 list of unmanned aircraft operator permit holders’ UAVs. The generalised UAV quadcopter was created using SolidWorks. Simulations were carried out with three different dimensions for the quadcopter, which were 290x290x200mm, 420x420x200mm, and 558x558x200mm. Two different camera position was also used for the simulation, mounted at the front and mounted at the center. Impact positions were chosen to be frontal impact and top impact. Impact velocity was fixed to 16m/s. The Impact Force Criterion was utilised to obtain the Abbreviated Injury Severity (AIS) for the impact scenarios. The results show that as the quadcopter dimensions increased, the contact forces on the human neck increased. However, when the quadcopter dimensions were smaller than the size of the human head, the contact force was at its highest due to the motors impacting the head directly. Furthermore, when the camera is mounted at the front, the impact force is greater than that mounted at the center. However, it should be noted that the rotation of the motor blades was not included in this study, which would affect the results. Further studies are required to consider the rotation of the motor blades impacting the human head and physical experiment is required to validate the study. Bachelor of Engineering (Mechanical Engineering) 2023-05-26T12:49:31Z 2023-05-26T12:49:31Z 2023 Final Year Project (FYP) Suresh S/O Ravi (2023). Collision severity evaluation of quadcopter UAV crash on human head. Final Year Project (FYP), Nanyang Technological University, Singapore. https://hdl.handle.net/10356/167408 https://hdl.handle.net/10356/167408 en application/pdf Nanyang Technological University
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Aeronautical engineering::Aircraft
Engineering::Mathematics and analysis::Simulations
spellingShingle Engineering::Aeronautical engineering::Aircraft
Engineering::Mathematics and analysis::Simulations
Suresh S/O Ravi
Collision severity evaluation of quadcopter UAV crash on human head
description This study focuses on determining the collision severity of a generalised quadcopter Unmanned Aerial Vehicle (UAV) crash on the human head. Finite Element Analysis (FEA) and explicit dynamics simulations on ABAQUS were used to determine the peak impact force. In this study, appropriate dimensions for the modelling of a generalised quadcopter UAV were obtained from dimensional analysis on Civil Aviation Authority of Singapore (CAAS) 2022 list of unmanned aircraft operator permit holders’ UAVs. The generalised UAV quadcopter was created using SolidWorks. Simulations were carried out with three different dimensions for the quadcopter, which were 290x290x200mm, 420x420x200mm, and 558x558x200mm. Two different camera position was also used for the simulation, mounted at the front and mounted at the center. Impact positions were chosen to be frontal impact and top impact. Impact velocity was fixed to 16m/s. The Impact Force Criterion was utilised to obtain the Abbreviated Injury Severity (AIS) for the impact scenarios. The results show that as the quadcopter dimensions increased, the contact forces on the human neck increased. However, when the quadcopter dimensions were smaller than the size of the human head, the contact force was at its highest due to the motors impacting the head directly. Furthermore, when the camera is mounted at the front, the impact force is greater than that mounted at the center. However, it should be noted that the rotation of the motor blades was not included in this study, which would affect the results. Further studies are required to consider the rotation of the motor blades impacting the human head and physical experiment is required to validate the study.
author2 Low Kin Huat
author_facet Low Kin Huat
Suresh S/O Ravi
format Final Year Project
author Suresh S/O Ravi
author_sort Suresh S/O Ravi
title Collision severity evaluation of quadcopter UAV crash on human head
title_short Collision severity evaluation of quadcopter UAV crash on human head
title_full Collision severity evaluation of quadcopter UAV crash on human head
title_fullStr Collision severity evaluation of quadcopter UAV crash on human head
title_full_unstemmed Collision severity evaluation of quadcopter UAV crash on human head
title_sort collision severity evaluation of quadcopter uav crash on human head
publisher Nanyang Technological University
publishDate 2023
url https://hdl.handle.net/10356/167408
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