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首页> 外文期刊>Unmanned Systems >Design and Fabrication of a Dual Rotor-Embedded Wing Vertical Take-Off and Landing Unmanned Aerial Vehicle
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Design and Fabrication of a Dual Rotor-Embedded Wing Vertical Take-Off and Landing Unmanned Aerial Vehicle

机译：双转子嵌入式翼垂直起飞和着陆无人机车辆的设计和制作

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摘要

The interest in building hybrid Unmanned Aerial Vehicles (UAVs) is increasing intensively due to its capability to perform Vertical Take-Off and Landing (VTOL), in addition to forward flight. With this capability, the hybrid UAVs are highly on demand in various industries. In this paper, a fixed-wing VTOL UAV with a novel configuration of a dual rotor-embedded wing was designed and developed. The methodology used in the design process adopted the traditional sizing and aerodynamic estimation method with advanced computational simulations and estimation approaches. The design was determined based on a thorough analysis of weight contribution, aerodynamics, propulsion, and stability and control. The results show that the UAV's preliminary design has successfully reached a total weight of 1.318 kg, achieved a high lift-to-drag ratio of approximately 4, and ensured stable flights with Level 1 flying qualities. A fixed-wing VTOL prototype was developed and fabricated based on the final design parameters using a low-cost hand lay-up process.
机译：由于其能够进行垂直起飞和降落（VTOL），因此除了向前飞行之外，对建筑混合的无人驾驶飞行器（无人机）的兴趣正在增加。通过这种功能，混合动力UAV在各个行业的需求量都是高度需求。在本文中，设计并开发了一种具有双转子嵌入式机翼的新配置的固定翼VTOL UAV。设计过程中使用的方法采用了具有高级计算模拟和估计方法的传统尺寸和空气动力学估计方法。该设计是基于对重量贡献，空气动力学，推进和稳定性和控制的彻底分析。结果表明，UAV的初步设计成功达到了1.318公斤的总重量，实现了大约4的高升力比，并确保了1级飞行质量的稳定飞行。使用低成本的手放置过程基于最终设计参数开发和制造固定翼VTOL原型。

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  • 来源
    《Unmanned Systems》 |2021年第1期|45-63|共19页
  • 作者

    Seng Man Wong; Hann Woei Ho; Mohd Zulkifly Abdullah;

  • 作者单位

    School of Aerospace Engineering Universiti Sains Malaysia Engineering Campus Nibong Tebal Penang 14300 Malaysia;

    School of Aerospace Engineering Universiti Sains Malaysia Engineering Campus Nibong Tebal Penang 14300 Malaysia Control and Simulation Faculty of Aerospace Engineering Delft University of Technology Kluyverweg 1 Delft 2629HS The Netherlands;

    School of Aerospace Engineering Universiti Sains Malaysia Engineering Campus Nibong Tebal Penang 14300 Malaysia;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Vertical Take-off and Landing; Unmanned Aerial Vehicles; Preliminary Design; Composite Wing Fabrication;

    机译：垂直起飞和着陆;无人驾驶车辆;初步设计;复合翼制造;

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