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Aerial platform attitude measurement by artificial vision

机译:人工视觉测量空中平台姿态

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摘要

Two measurement systems based on electronic imagers for attitude determination of light and low-cost airborne vectors in clear weather condition are presented. Both the devices are based on the following scheme: a binarized sky line image is selected as referential, then each shot, after binarization is segmented in two parts whose mean values are subtracted to the corresponding data computed from referential image. From this comparison analogical or digital values are deduced that give way to estimating the roll and pitch variation angles. The first system is made of off-the-shelf devices: black and white CMOS camera and processing unit made of a dedicated electronic. A second proposition is presented. It makes use of a CMOS retina, developed by our team, dedicated to real time, analogical intercorrelation computing. A simple external processing implemented in a microcontroller completes the system. A model for the embarked imaging system and an equation for an ideal horizon image with respect to rolling and pitch angles are proposed. The method for estimating these angles from the image and errors induced by the various approximations of the model are then presented. A series of experimental results obtained from real images confirms the previous propositions. The last section is dedicated to a presentation of the retinal imager solution, experimental results are also provided in this part.
机译:提出了两种基于电子成像仪的测量系统,用于在晴朗天气条件下确定光和低成本机载矢量的姿态。两种设备均基于以下方案:选择二值化的天空线图像作为参考,然后在二值化后将每个镜头分为两部分,将其平均值减去从参考图像计算出的相应数据。从该比较中推导出类比或数字值,该类比或数字值让位于估计侧倾和俯仰变化角。第一个系统由现成的设备组成:黑白CMOS相机和专用电子设备制成的处理单元。提出了第二个命题。它利用了我们团队开发的CMOS视网膜,专门用于实时,模拟互相关计算。通过微控制器实现的简单外部处理即可完善系统。提出了用于登载成像系统的模型以及关于滚动角和俯仰角的理想水平图像的方程。然后介绍了从图像估计这些角度的方法以及由模型的各种近似值引起的误差。从真实图像获得的一系列实验结果证实了先前的主张。最后一部分专门介绍了视网膜成像仪解决方案,该部分还提供了实验结果。

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