Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/169194
Title: Collision severity analysis of quadrotors on covered linkways for ground risk assessment in urbanized environments
Authors: Mohd Hasrizam Che Man
Sivakumar, Anush Kumar
Ng, Nathaniel Jingwei
Low, Kin Huat 
Keywords: Engineering::Aeronautical engineering::Aviation
Engineering::Aeronautical engineering::Accidents and air safety
Issue Date: 2023
Source: Mohd Hasrizam Che Man, Sivakumar, A. K., Ng, N. J. & Low, K. H. (2023). Collision severity analysis of quadrotors on covered linkways for ground risk assessment in urbanized environments. AIAA AVIATION 2023 Forum. https://dx.doi.org/10.2514/6.2023-4413
Conference: AIAA AVIATION 2023 Forum
Abstract: With the promise to revolutionize many industries, the popularity of Unmanned Aerial Vehicles (UAVs) has surged in the last two decades. The use of multirotor UAVs in urban areas is gaining traction, with applications such as cargo delivery, emergency response, and recreational flight. However, unlike manned aviation, UAVs do not have a standardized design, testing, and certification procedures. Hence, a lot of countries raised their concerns about the risk of potential multi-rotor UAV crashes and impacting pedestrians on the ground. Apart from high-rise buildings, covered linkways are a ubiquitous sight in countries like Singapore with a primary role to provide shelter for pedestrians in the event of rain. Therefore, this study investigates the collision severity of a multirotor UAV impacting a covered linkway. Briefly put, the level of protection that covered linkways can provide to pedestrians from a multirotor UAV falling from height is analyzed. The methodology in this study is divided into three phases. In Phase 1, Finite Element Analysis (FEA) is employed to simulate the impact of two specific multirotor UAV designs and solid spheres with comparable material properties as they collide onto a simplified covered linkway panel using ABAQUS/CAE. Subsequently, parametric analysis using Python scripting is performed to assess the collision severity due to variations in mass and crash speed of rigid sphere. Phases 2 and 3 explore the impact of the honeycomb structure modelling on the impact simulation. Findings from this study will be beneficial for the computation of sheltering factor in UAV ground risk assessment.
URI: https://hdl.handle.net/10356/169194
DOI: 10.2514/6.2023-4413
Schools: School of Mechanical and Aerospace Engineering 
Research Centres: Air Traffic Management Research Institute 
Rights: © 2023 American Institute of Aeronautics and Astronautics, Inc. All rights reserved. This paper was published in the Proceedings of AIAA AVIATION 2023 Forum and is made available with permission of American Institute of Aeronautics and Astronautics, Inc.
Fulltext Permission: open
Fulltext Availability: With Fulltext
Appears in Collections:ATMRI Conference Papers
MAE Conference Papers

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