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Fixed-Wing Attitude Estimation Using Computer Vision Based Horizon Detection

机译:使用基于计算机视觉的水平检测的固定翼姿态估计

摘要

The last decade has seen a dramatic expansion in the deployment of Unmanned Airborne Vehicles (UAVs) as witnessed by deployments to Bosnia, Afghanistan and Iraq. Many low-cost UAVs operate without redundant attitude sensors and are therefore highly vulnerable to the failure of such sensors. ududIt is common for low-cost UAVs to carry a vision sensor as its primary payload. Given that a human pilot is trained to control an aircraft with respect to a visual horizon under Visual Meteorological Conditions (VMC), it is logical to suggest that a similar capability be developed for a UAV in the event of the failure of the primary attitude system. In addition, it potentially gives the capability to estimate the attitude of a gimballed camera, without specifically equipping the gimballed platform with an angular sensor.ududIn this paper, we develop a method for estimating the flight critical parameters of pitch angle, roll angle and the three body rates using horizon detection and optical flow. We achieve this through the use of an image processing front-end to detect candidate horizon lines through the use of morphological image processing and the Hough transform. The optical flow of the image for each candidate line is calculated, and using these measurements, we are able to estimate the body rates of the aircraft. Using an Extended Kalman Filter (EFK), the candidate horizon lines are propagated and tracked through successive image frames, with statistically unlikely horizon candidates eliminated. ududResults are shown for a number of different datasets taken with cameras ranging from low-cost webcams to high-quality machine vision cameras are presented. Preliminary results show that although the front-end is adequate in many different scenarios, utilising temporal information results in a more robust performance of the detection algorithm which is well suited for use in attitude estimation.
机译:在过去的十年中,无人驾驶飞行器(UAV)的部署有了显着扩展,向波斯尼亚,阿富汗和伊拉克的部署见证了这一点。许多低成本的无人机在没有冗余姿态传感器的情况下运行,因此极易受到此类传感器故障的影响。 ud ud低成本无人机通常会将视觉传感器作为其主要有效载荷。假设在视觉气象条件(VMC)下训练了一名飞行员来控制飞机相对于视界的水平,那么逻辑上建议在主姿态系统发生故障的情况下为无人机开发类似的能力。此外,它可能能够估算万向摄像机的姿态,而无需专门为万向平台配备角度传感器。 ud ud本文中,我们开发了一种估算俯仰角,侧倾角的飞行关键参数的方法角度和三个身体速率使用水平检测和光流。我们通过使用图像处理前端通过使用形态图像处理和霍夫变换来检测候选视线来实现这一点。计算每条候选线的图像的光流,并使用这些测量值,我们能够估算飞机的机体速率。使用扩展卡尔曼滤波器(EFK),可以在连续的图像帧中传播和跟踪候选地平线,并在统计上消除了不可能的地平线候选。 ud ud显示了从低成本网络摄像头到高质量机器视觉相机的各种相机拍摄的不同数据集的结果。初步结果表明,尽管前端在许多不同的场景中都是足够的,但利用时间信息可以使检测算法具有更强大的性能,非常适合用于姿态估计。

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