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Safety Assessment and Risk Estimation for Unmanned Aerial Vehicles Operating in National Airspace System

机译:在国家空域系统中运行的无人机的安全评估和风险估计

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摘要

This paper proposes an effective approach for modelling and assessing the risks associated with unmanned aerial vehicles (UAVs) integrated into national airspace system (NAS). Two critical hazards with UAV operations are considered and analyzed, which are ground impacts and midair collisions. Threats to fatalities that result from the two hazards are the focus in the proposed method. In order to realize ground impact assessment, a multifactor risk model is designed by calculating system reliability required to meet a target level of safety for different UAV categories. Both fixed-wing and rotary-wing UAVs are taken into account under a real scenario that is further partitioned into different zones to make the evaluation more precise. Official territory and population data of the operation scenario are incorporated, as well as UAV self-properties. Casualty area of impacting debris can be obtained as well as the probability of fatal injuries on the ground. Sheltering factors are not neglected and defined as four types based on the real scenario. When midair collision fatality risk is estimated, a model of aircraft collisions based on the density of civil flight in different regions over Chinese airspace is proposed. In the model, a relative collision area and flying speed between UAVs and manned aircraft are constructed to calculate expected frequency of fatalities for each province correspondingly. Truthful data with different numbers of UAVs is incorporated in the model with the expected number of fatalities after a collision is included. Experimental simulations are made to evaluate the ground impacts and midair collisions when UAVs operate in the NAS.
机译:本文提出了一种有效的方法,用于建模和评估与整合到国家空域系统(NAS)中的无人机(UAV)相关的风险。考虑并分析了无人机操作的两个关键危害,即地面撞击和空中碰撞。由这两种危害导致的死亡威胁是所提出方法的重点。为了实现地面影响评估,通过计算满足不同无人机类别的安全目标水平所需的系统可靠性来设计多因素风险模型。在实际情况下,固定翼和旋转翼无人机都被考虑在内,并进一步划分为不同区域,以使评估更加精确。合并了作战方案的官方领土和人口数据,以及无人机的自身属性。可以获得撞击碎片的伤亡面积以及在地面上造成致命伤害的可能性。不应忽略庇护因素,而是根据实际情况将庇护因素定义为四种类型。在估算空中撞机致死危险时,提出了一种基于中国领空不同地区民用飞行密度的飞机撞机模型。在该模型中,构建了无人机与有人驾驶飞机之间的相对碰撞区域和飞行速度,以相应地计算每个省的预期死亡人数。模型中包含了具有不同数量的无人机的真实数据,并包含了碰撞后的预期死亡人数。当无人机在NAS中运行时,进行了实验仿真以评估地面撞击和空中碰撞。

著录项

  • 来源
    《Journal of Advanced Transportation》 |2018年第6期|4731585.1-4731585.11|共11页
  • 作者单位

    Xihua Univ Sch Automobile & Transportat Chengdu Sichuan Peoples R China|Beihang Univ Sch Elect & Informat Engn Beijing Peoples R China;

    Beihang Univ Sch Elect & Informat Engn Beijing Peoples R China|Shandong Jiaotong Univ Sch Informat Sci & Elect Engn Jinan Shandong Peoples R China;

    Univ S Florida Dept Civil & Environm Engn Tampa FL USA;

    Civil Aviat Management Inst China Sch Gen Aviat Beijing Peoples R China;

    Ecole Natl Aviat Civile MAIAA Lab Toulouse France;

    Xihua Univ Sch Automobile & Transportat Chengdu Sichuan Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-18 05:03:39

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