...
  • 主题
高级搜索  >
历史搜索 清空历史
首页> 外文期刊>Journal of robotics >Analysis on Hover Control Performance of T- and Cross-Shaped Tail Fin of X-Wing Single-Bar Biplane Flapping Wing
【24h】

Analysis on Hover Control Performance of T- and Cross-Shaped Tail Fin of X-Wing Single-Bar Biplane Flapping Wing

机译：X翼单条双翼形翼片翼翅片悬停控制性能分析

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

摘要

The current flapping wing adopts T-shaped or cross-shaped tail fin to adjust its flight posture. However, how the tail fin will affect the hover control is not very clear. So, the effects of the two types of tail on flight will be analyzed and compared by actual flight tests in this paper. Firstly, we proposed a new X-wing single-bar biplane flapping-wing mechanism with two pairs of wings. Thereafter, the overall structure, gearbox structure, tail, frame, and control system of the flapping wing were designed and analyzed. Secondly, the control mechanism of hover is analyzed to describe the effect of two-tail fin on posture control. Thirdly, the Beetle was used as the control unit to achieve a controllable flight of flapping wing. The MPU6050 electronic gyroscope was used to monitor the drone’s posture in real time, and the Bluetooth BLE4.0 wireless communication module was used to receive remote control instructions. At last, to verify the flight effect, two actual flapping wings were fabricated and flight experiments were conducted. The experiments show that the cross-shaped tail fin has a better controllable performance than the T-shaped tail fin. The flapping wing has a high lift-to-mass ratio and good maneuverability. The designed control system can achieve the controllable flight of the flapping wing.
机译：目前的拍打翼采用T形或横形尾鳍来调节其飞行姿势。但是，尾鳍将如何影响悬停控制并不是很清楚。因此，通过本文的实际飞行试验将分析两种类型的飞行尾部的效果。首先，我们提出了一种具有两对翼的新X-Wing单杠双翼形翼翼机构。此后，设计并分析了扑翼翼的整体结构，变速箱结构，尾部，框架和控制系统。其次，分析了悬停的控制机制，描述了双尾鳍对姿势控制的影响。第三，甲虫被用作控制单元，以实现可控制的拍打飞行。 MPU6050电子陀螺仪用于实时监测无人机的姿势，使用蓝牙BLE4.0无线通信模块接收远程控制指令。最后，为了验证飞行效果，制造了两种实际拍打翅膀，并进行飞行实验。实验表明，十字形尾鳍具有比T形尾部更好的可控性能。拍打翼具有高升力比率和良好的机动性。设计的控制系统可以实现扑翼的可控飞行。

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