Prediction of Sensor Performance Required for Reliable Aircraft Target Discrimination

D. Parker, Henry White, J. Oakley, G. Bishop
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Abstract

For new military aircraft a specification of sensor characteristics and performance is required at an early stage in the design cycle, well before testing of a prototype. In the early days of military aviation the Johnson criteria [1] were used to determine the sensor resolution required for target recognition by a human. In the present day sensor data are processed by computer using various Automatic Target Recognition (ATR) algorithms. However there is no accepted method for predicting the sensor resolution and SNR required for reliable ATR and hence there is risk that any chosen sensor may fail to support the required ATR performance. This paper reports a study into the use of publicly-available CAD models for aircraft to address this requirement. The study considers the worst-case confusion between two views of 15 different aircraft types. For simplicity only rotations by an angle θ about the Z (vertical) axis are considered. Firstly the sensor resolution and noise level is fixed. Then for each aircraft type and view angle an ensemble of synthetic silhouettes are generated. Using these ensembles, a-posteriori distributions of 5 standard scale-invariant shape features (eccentricity, orientation, solidity, circularity and bounding box aspect ratio) are estimated for each view angle θ. The performance of ATR at the given resolution and noise level is predicted by estimating the Bayes Error Rate [2] when deciding between each aircraft type and the 14 non-matching types using these features. The worst-case confusion in terms of erroneous aircraft type and view angle is identified. The sensor resolution is then changed and the above process repeated to investigate the effect of varying sensor resolution on performance. As expected, high sensor resolution leads to low probability of misclassification, even in the worst-case. Reduction in resolution and increasing noise level causes the Bayes Error Rate to rise quickly. The Bayes Error Rate gives a fundamental limit to the reliability of classification, irrespective of the actual type of classification algorithm used. The predictions from the model are confirmed by testing against a standard classifier for specific discrimination examples. Further development of the approach presented is expected to yield a method for specifying sensor resolution requirements for specific ATR problems.
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可靠飞机目标识别所需传感器性能预测
对于新型军用飞机来说,在设计周期的早期阶段,在原型机测试之前,就需要对传感器特性和性能进行规范。在军事航空的早期,约翰逊标准[1]被用来确定人类目标识别所需的传感器分辨率。目前,传感器数据由计算机处理,使用各种自动目标识别(ATR)算法。然而,没有公认的方法来预测可靠的ATR所需的传感器分辨率和信噪比,因此存在任何选择的传感器可能无法支持所需的ATR性能的风险。本文报告了一项使用公开可用的飞机CAD模型来解决这一要求的研究。该研究考虑了15种不同飞机类型的两种视图之间最坏的混淆。为简单起见,只考虑绕Z(垂直)轴旋转一个角度θ。首先确定传感器的分辨率和噪声水平。然后,对于每种飞机类型和视角,生成合成轮廓的集合。利用这些集合,估计了每个视角θ下5个标准尺度不变形状特征(偏心率、方向、固体度、圆度和边界框宽高比)的后验分布。ATR在给定分辨率和噪声水平下的性能是通过估计贝叶斯错误率[2]来预测的,当使用这些特征在每种飞机类型和14种不匹配的飞机类型之间做出决定时。在错误的飞机类型和视角方面,确定了最坏情况下的混淆。然后改变传感器分辨率,重复上述过程以研究不同传感器分辨率对性能的影响。正如预期的那样,高传感器分辨率导致即使在最坏的情况下,错误分类的概率也很低。分辨率的降低和噪声水平的增加导致贝叶斯误差率迅速上升。贝叶斯错误率对分类的可靠性给出了一个基本的限制,而不考虑实际使用的分类算法类型。模型的预测通过针对特定判别示例的标准分类器进行测试来证实。所提出的方法的进一步发展有望产生一种针对特定ATR问题指定传感器分辨率要求的方法。
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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