Evaluation of Neural Network Verification Methods for Air-to-Air Collision Avoidance

Q2 Social Sciences
Diego Manzanas Lopez, Taylor T. Johnson, Stanley Bak, Hoang-Dung Tran, Kerianne L. Hobbs
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引用次数: 4

Abstract

Neural network approximations have become attractive to compress data for automation and autonomy algorithms for use on storage-limited and processing-limited aerospace hardware. However, unless these neural network approximations can be exhaustively verified to be safe, they cannot be certified for use on aircraft. An example of such systems is the unmanned Airbone Collision Avoidance System (ACAS Xu), which is a very popular benchmark for open-loop neural network control system verification tools. This paper proposes a new closed loop extension of this benchmark, which consists of a set of ten closed loop properties selected to evaluate the safety of an ownship aircraft in the presence of a co-altitude intruder aircraft. These closed loop safety properties are used to evaluate 5 of the 45 neural networks that comprise the ACAS Xu benchmark (corresponding to co-altitude cases) as well as the switching logic between the 5 neural networks. The combination of nonlinear dynamics and switching between five neural networks is a challenging verification task accomplished with star set reachability methods in two verification tools. The safety of the ownship aircraft under initial position uncertainty is guaranteed in every scenario proposed. using the NNV and nnenum tools on 5 of 45 ACAS Xu neural networks with switching between five to co-altitude collision cases. Both tools show reachable states of an ownship with dynamics on a collision course with an intruder The reachability computation and ownship by 5 switched NNs. The verification switch collision free even a large initial This study showed that do a comprehensive safety verification analysis of a complex air collision advisory system for but further research determine flights In the tool showed and computation
空对空避碰的神经网络验证方法评价
神经网络近似对于压缩数据以用于存储受限和处理受限的航空航天硬件的自动化和自主算法已经变得很有吸引力。然而,除非这些神经网络近似能够被彻底证明是安全的,否则它们不能被确定用于飞机。此类系统的一个例子是无人驾驶的Airbone防撞系统(ACAS Xu),它是开环神经网络控制系统验证工具的一个非常流行的基准。本文提出了该基准的一个新的闭环扩展,该扩展由一组10个闭环特性组成,这些特性被选择来评估在同高度入侵飞机存在的情况下本船飞机的安全性。这些闭环安全特性用于评估45个神经网络中的5个,这些神经网络包括ACAS-Xu基准(对应于同高度情况)以及5个神经网络之间的切换逻辑。非线性动力学和五个神经网络之间的切换的结合是一项具有挑战性的验证任务,使用两种验证工具中的星集可达性方法来完成。在提出的每一种方案中,都保证了在初始位置不确定的情况下本船飞机的安全。在45个ACAS-Xu神经网络中的5个上使用NNV和NNnum工具,在五个到同高度碰撞情况之间切换。这两个工具都显示了本船在与入侵者碰撞过程中的可达状态。5个切换NN的可达性计算和本船。验证开关无碰撞,甚至是一个大型的初始验证。该研究表明,对复杂的空中碰撞咨询系统进行了全面的安全验证分析,但进一步的研究确定了所示工具和计算中的缺陷
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
Journal of Air Transportation
Journal of Air Transportation Social Sciences-Safety Research
CiteScore
2.80
自引率
0.00%
发文量
16
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