| 注册
首页|期刊导航|南京航空航天大学学报(英文版)|轻型无人机与飞机风挡碰撞风险研究

轻型无人机与飞机风挡碰撞风险研究

张柱国 陆晓华 张迎春 李玉龙 张洪海

南京航空航天大学学报(英文版)2023,Vol.40Issue(5):534-546,13.
南京航空航天大学学报(英文版)2023,Vol.40Issue(5):534-546,13.DOI:10.16356/j.1005-1120.2023.05.003

轻型无人机与飞机风挡碰撞风险研究

Research on Collision Risk Between Light Unmanned Arial Vehicles and Aircraft Windshield

张柱国 1陆晓华 2张迎春 3李玉龙 4张洪海2

作者信息

  • 1. 西北工业大学航空学院, 西安 710072,中国||中国民航上海航空器适航审定中心, 上海 200335,中国
  • 2. 南京航空航天大学民航学院, 南京 211106,中国
  • 3. 中国民航上海航空器适航审定中心, 上海 200335,中国
  • 4. 西北工业大学航空学院, 西安 710072,中国
  • 折叠

摘要

Abstract

With the increasing unmanned aerial vehicles(UAVs)applications,quite a few major aviation incidents and dangerous symptoms have occurred in the vicinity of the airport and the airspace,and air transportation safety is facing a huge potential threat from unorder flight of UAVs.An important aspect regarding the collision risk between a typical UAV and the windshield of a commercial aircraft is investigated.The damage classification and corresponding impact energy range considering the weakest area on the aircraft windshield are obtained via finite element simulation under the most severe condition.According to the simulation results,the damage severity rank can be classified conservatively.In the absence of intervention from air traffic control,Monte Carlo simulation is performed to obtain the collision probability between a UAV and an aircraft with their independent motions by considering the joint constraints of the minimum horizontal safety separation,the minimum lateral safety separation,and the minimum vertical safety separation.In addition,the collision probability levels are also estimated.Based on various combinations of damage severity classifications and collision probability levels,a more conservative qualitative risk matrix is defined regarding collision between a UAV and an aircraft windshield.In general,the results indicate that the collision risk and damage severity are low when the UAV and the aircraft are flying at the height of less than 120 m and a distance of over 3600 m on the condition of a typical heading angle and a pitch angle,otherwise these factors become serious.This investigation would provide a theoretical basis and practical reference for the normative design and manufacture of UAVs,the policy formulation by authorities on UAV operation control,as well as the risk assessment of UAVs and manned aircraft operating in the same airspace.

关键词

无人机/飞机风挡/碰撞概率/损伤严重性/能量等级/风险矩阵

Key words

unmanned aerial vehicle(UAV)/aircraft windshield/collision probability/damage severity/energy level/risk matrix

分类

航空航天

引用本文复制引用

张柱国,陆晓华,张迎春,李玉龙,张洪海..轻型无人机与飞机风挡碰撞风险研究[J].南京航空航天大学学报(英文版),2023,40(5):534-546,13.

基金项目

This work was supported by the Na-tional Natural Science Foundation of China(No.71971114). (No.71971114)

南京航空航天大学学报(英文版)

OACSCDCSTPCD

1005-1120

访问量0
|
下载量0
段落导航相关论文