首页> 外文学位 >Vision based control of unmanned aerial vehicles with applications to an autonomous four-rotor helicopter, quadrotor.
【24h】

Vision based control of unmanned aerial vehicles with applications to an autonomous four-rotor helicopter, quadrotor.

机译:基于视觉的无人机控制,应用于自动四旋翼直升机,四旋翼飞机。

获取原文
获取原文并翻译 | 示例

摘要

Our work proposes a vision-based stabilization and output tracking control method for a model helicopter. This is a part of our effort to produce a rotorcraft based autonomous Unmanned Aerial Vehicle (UAV). Due to the desired maneuvering ability, a four-rotor helicopter has been chosen as the testbed. On previous research on flying vehicles, vision is usually used as a secondary sensor. Unlike previous research, our goal is to use visual feedback as the main sensor, which is not only responsible for detecting where the ground objects are but also for helicopter localization. A novel two-camera method has been introduced for estimating the full six degrees of freedom (DOF) pose of the helicopter. This two-camera system consists of a pan-tilt ground camera and an onboard camera. The pose estimation algorithm is compared through simulation to other methods, such as four-point, and stereo method and is shown to be less sensitive to feature detection errors. Helicopters are highly unstable flying vehicles; although this is good for agility, it makes the control harder. To build an autonomous helicopter, two methods of control are studied—one using a series of mode-based, feedback linearizing controllers and the other using a back-stepping control law. Various simulations with 2D and 3D models demonstrate the implementation of these controllers. We also show global convergence of the 3D quadrotor controller even with large calibration errors or presence of large errors on the image plane. Finally, we present initial flight experiments where the proposed pose estimation algorithm and non-linear control techniques have been implemented on a remote-controlled helicopter. The helicopter was restricted with a tether to vertical, yaw motions and limited x and y translations.
机译:我们的工作提出了一种用于模型直升机的基于视觉的稳定和输出跟踪控制方法。这是我们生产基于旋翼飞机的自主无人飞行器(UAV)的工作的一部分。由于具有理想的机动能力,因此选择了四旋翼直升机作为试验台。在先前对飞行器的研究中,视觉通常用作辅助传感器。与以前的研究不同,我们的目标是使用视觉反馈作为主要传感器,该传感器不仅负责检测地面物体的位置,而且还负责直升机的定位。引入了一种新颖的两摄像机方法来估计直升机的完整六自由度(DOF)姿势。该两摄像头系统由一个云台地面摄像头和一个车载摄像头组成。通过仿真将姿势估计算法与其他方法(例如四点和立体声方法)进行了比较,结果表明该方法对特征检测错误较不敏感。直升机是高度不稳定的飞行器;尽管这对敏捷性有好处,但它会使控制变得更加困难。为了制造自主直升机,研究了两种控制方法-一种使用一系列基于模式的反馈线性化控制器,另一种使用后退控制律。使用2D和3D模型进行的各种仿真演示了这些控制器的实现。我们还显示了3D四旋翼控制器的全局收敛性,即使存在较大的校准误差或图像平面上存在较大的误差也是如此。最后,我们介绍了最初的飞行实验,其中所提出的姿态估计算法和非线性控制技术已在遥控直升机上实现。直升飞机只能通过系绳进行垂直,偏航运动,并且 x y 的翻译受到限制。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号