• 主题
高级搜索  >
历史搜索 清空历史
首页> 外文会议>IEEE International Conference on Robotics and Automation >Development of a quad rotor tail-sitter VTOL UAV without control surfaces and experimental verification
【24h】

Development of a quad rotor tail-sitter VTOL UAV without control surfaces and experimental verification

机译：无控制面的四旋翼尾桨VTOL无人机的研制和实验验证

获取原文
页面导航
  • 摘要
  • 著录项
  • 相似文献
  • 相关主题

摘要

This paper presents development of a quad rotor tail-sitter VTOL UAV (Vertical Takeoff and Landing Unmanned Aerial Vehicle) which is composed of four rotors and a fixed wing. The conventional VTOL UAVs have a drawback in the accuracy of the attitude control in stationary hovering because they were developed based on a fixed-wing aircraft and they used the control surfaces, such as aileron, elevator, and rudder for the attitude control. To overcome such a drawback, we developed a quad rotor tail-sitter VTOL UAV. The quad rotor tail-sitter VTOL UAV realizes high accuracy in the attitude control with four rotors like a quad rotor helicopter and achieves level flight like a fixed-wing airplane. The remarkable characteristic of the developed quad rotor tail-sitter VTOL UAV is that it does not use any control surfaces even in the level flight. This paper shows the design concept of the developed UAV and experimental verification of all flight modes including hovering, transition flight and level flight.
机译：本文介绍了一种四旋翼尾翼垂直起降无人机（垂直起降无人飞行器），它由四个旋翼和一个固定翼组成。传统的VTOL无人机是基于固定翼飞机开发的，并且它们使用诸如副翼，升降舵和方向舵之类的控制表面进行姿态控制，因此在静态悬停时姿态控制的准确性存在缺陷。为了克服这一缺点，我们开发了四旋翼尾桨式VTOL UAV。四旋翼尾桨式VTOL无人机可以像四旋翼直升机那样通过四个旋翼实现高精度的姿态控制，并可以像固定翼飞机一样实现水平飞行。研制的四旋翼尾桨式VTOL UAV的显着特点是，即使在水平飞行中也不会使用任何控制面。本文展示了已开发的无人机的设计概念以及包括悬停，过渡飞行和水平飞行在内的所有飞行模式的实验验证。

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