A comparison of two novel approaches for conducting detect and avoid flight test

IF 1.3 Q3 REMOTE SENSING
K. Ellis, Iryna Borshchova, S. Jennings, Caidence Paleske
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引用次数: 1

Abstract

This paper compares two approaches developed by the National Research Council of Canada to conduct “near-miss” intercepts in flight test, and describes a new method for assessing the efficacy of these trajectories. Each approach used a different combination of flight test techniques and displays to provide guidance to the pilots to set-up the aircraft on a collision trajectory and to maintain the desired path. Approach 1 only provided visual guidance of the relative azimuth and position of the aircraft, whereas Approach 2 established the conflict point (latitude/longitude) from the desired geometry, and provided cross track error from the desired intercept as well as speed cueing for the arrival time. The performance of the approaches was analyzed by comparing the proportion of time where the predicted closest approach distance was below a desired threshold value. The analysis showed that Approach 2 resulted in more than double the amount of time spent at or below desired closest approach distance across all azimuths flown. Moreover, since less time was required to establish the required initial conditions, and to stabilize the flight paths, the authors were able to conduct 50% more intercepts.
两种新的探测和规避飞行试验方法的比较
本文比较了加拿大国家研究委员会开发的两种在飞行试验中进行“未遂”拦截的方法,并描述了一种评估这些轨迹有效性的新方法。每种方法都使用了飞行测试技术和显示器的不同组合,为飞行员提供指导,以将飞机设置在碰撞轨迹上并保持所需的路径。进近1只提供了飞机相对方位角和位置的视觉引导,而进近2根据所需几何形状确定了冲突点(纬度/经度),并提供了所需截距的交叉航迹误差以及到达时间的速度提示。通过比较预测的最接近接近距离低于所需阈值的时间比例,分析了这些方法的性能。分析表明,进近2导致在所有飞行方位上处于或低于所需最接近进近距离的时间增加了一倍多。此外,由于建立所需的初始条件和稳定飞行路径所需的时间较少,作者能够进行50%以上的拦截。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
5.30
自引率
0.00%
发文量
2
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