论文标题

一种基于视觉的控制方法,用于在不使用GPS的情况下自动着陆垂直飞行飞机在移动平台上

A Vision-Based Control Method for Autonomous Landing of Vertical Flight Aircraft On a Moving Platform Without Using GPS

论文作者

Lee, Bochan, Saj, Vishnu, Benedict, Moble, Kalathil, Dileep

论文摘要

本文讨论了一种基于视力的估计和控制方法,以实现垂直起飞和着陆(VTOL)在移动平台上的无人驾驶飞机(VTOL)的完全自主跟踪和着陆,而无需依赖GPS信号。当前方法的一个独特功能是,它可以完成此任务,而无需跟踪降落垫本身。但是,通过利用标准化的视觉提示安装在降落板上,并平行于飞行员/车辆的视线。开发了使用单眼相机的计算机视觉系统来检测视觉提示,然后准确估算无人机的标题及其在所有三个方向上的相对距离。通过与基于维孔的运动捕获系统进行比较,展示了本视觉系统实时测量距离的能力,其精度在小于厘米的精度范围内,并在一定程度的范围内与正确的视觉提示进行了趋势。增益 - 安排的比例积分衍生物(PID)控制系统与视觉系统集成在一起,然后在称为Guazebo的逼真的仿真程序中在Quad-Rotor-UAV动态模型上实现。进行了广泛的模拟,以证明控制器实现可靠的跟踪并降落在任意轨迹上的平台上的能力。使用固定平台和移动平台的重复飞行测试成功地进行了不到5厘米的着陆误差。

The paper discusses a novel vision-based estimation and control approach to enable fully autonomous tracking and landing of vertical take-off and landing (VTOL) capable unmanned aerial vehicles (UAVs) on moving platforms without relying on a GPS signal. A unique feature of the present method is that it accomplishes this task without tracking the landing pad itself; however, by utilizing a standardized visual cue installed normal to the landing pad and parallel to the pilot's/vehicle's line of sight. A computer vision system using a single monocular camera is developed to detect the visual cue and then accurately estimate the heading of the UAV and its relative distances in all three directions to the landing pad. Through comparison with a Vicon-based motion capture system, the capability of the present vision system to measure distances in real-time within an accuracy of less than a centimeter and heading within a degree with the right visual cue, is demonstrated. A gain-scheduled proportional integral derivative (PID) control system is integrated with the vision system and then implemented on a quad-rotor-UAV dynamic model in a realistic simulation program called Gazebo. Extensive simulations are conducted to demonstrate the ability of the controller to achieve robust tracking and landing on platforms moving in arbitrary trajectories. Repeated flight tests, using both stationary and moving platforms are successfully conducted with less than 5 centimeters of landing error.

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