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Total system error performance of drones for an unmanned PBN concept

机译:无人驾驶PBN概念的无人机的总系统错误性能

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The German Aerospace Center (DLR) operates small drones i.e., octocopters for research purposes at different institutions at different locations. In addition, the DLR is working on the integration of drones into unsegregated airspace in several national and international projects. One of the key elements for a safe integration of drones is the positioning capability of the air vehicle. On the one hand it is required for geofencing applications in order to create no-fly zones and on the other hand it is required to generate an airspace management for unmanned traffic. In recent years, the Performance Based Navigation (PBN) concept was introduced for manned aviation to exploit the navigation performance of modern satellite navigation and to manage the available airspace. One approach for Unmanned Aircraft System (UAS) Traffic Management (UTM) is obviously to transfer the PBN concept for drone applications. However, as drones usually use commercial off the shelf equipment that is usually not certified for aviation applications, the question is how the basic principle can be transferred. In this work, we used a commercial octocopter (MikroKopter MK Okto XL 6S12 ARF) to assess the horizontal Navigation System Error (NSE) as well as the lateral Total System Error (TSE) while using different GNSS receivers. The horizontal navigation is based on GNSS in stand-alone mode or using SBAS augmentation and a compass for directional information aid. No additional sensors like inertial measurements are used here. We are going to present the results from flight trials with two different GNSS receivers and will draw conclusions for a PBN concept for drones.
机译:德国航空航天中心(DLR)在不同地点的不同机构中运行小型无人机,即八旋翼飞行器,以进行研究。此外,DLR正在几个国家和国际项目中致力于将无人机整合到未隔离的空域中。无人机安全整合的关键要素之一是飞行器的定位能力。一方面,地理围栏应用程序需要创建禁飞区,另一方面,它需要为无人驾驶交通生成空域管理。近年来,有人驾驶航空引入了基于性能的导航(PBN)概念,以利用现代卫星导航的导航性能并管理可用空域。无人机系统(UAS)交通管理(UTM)的一种方法显然是将PBN概念转移到无人机应用中。但是,由于无人机通常使用通常没有经过航空认证的现成的商用设备,因此问题在于如何转移基本原理。在这项工作中,当使用不同的GNSS接收器时,我们使用了商用八旋翼飞机(MikroKopter MK Okto XL 6S12 ARF)来评估水平导航系统误差(NSE)和横向总系统误差(TSE)。水平导航基于GNSS的独立模式,或者使用SBAS增强功能和指南针来提供方向信息。此处不使用惯性测量等其他传感器。我们将介绍使用两个不同的GNSS接收器进行的飞行试验的结果,并将得出针对无人机的PBN概念的结论。

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