Design of a Lift-propulsion VTOL UAV system

机译：升力推进式垂直起降无人机系统的设计

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In this paper, a general design method for lift-propulsion vertical take-off and landing unmanned aerial vehicle (VTOL UAV) is proposed. The power matching based conceptual parameter estimation and aerodynamic shape design are carried out. The attitude control law is designed. The hovering and level flight test of the prototype are carried out. Confirming the validity of the overall design method and the attitude control law design.

机译：提出了一种提升推进垂直起降无人机的通用设计方法。进行了基于功率匹配的概念参数估计和空气动力学形状设计。设计了姿态控制律。进行了原型的悬停和水平飞行测试。确认总体设计方法和姿态控制律设计的有效性。

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《IEEE International Conference on Mechatronics and Automation》|2018年|1908-1913|共6页
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Xin Zhao; Zhou Zhou; Xiaoping Zhu;
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关键词
Fans; Aircraft; Propellers; Fuels; Engines; Automotive components;

机译：风扇;飞机;螺旋桨;燃料;发动机;汽车零部件;

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专利

1. DESIGN AND EXPERIMENT OF A HIGH PAYLOAD FIXED WING VTOL UAV SYSTEM FOR EMERGENCY RESPONSE [J] . H. Wu, Z. Wang, B. Ren, International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences . 2020,第4期

机译：高效载荷固定翼VTOL UAV系统进行紧急响应的设计与实验
2. Systematic design methodology for development and flight testing of a variable pitch quadrotor biplane VTOL UAV for payload delivery [J] . Chipade Vishnu S., Abhishek, Kothari Mangal, Mechatronics: The Science of Intelligent Machines . 2018,第期

机译：用于有效载荷传递的可变间距四轮运动双向VTOL UAV的系统设计方法
3. Design of a Commercial Hybrid VTOL UAV System [J] . Ugur Ozdemir, Yucel Orkut Aktas, Aslihan Vuruskan, Journal of Intelligent & Robotic Systems: Theory & Application . 2014,第1a2期

机译：商用混合动力垂直起降无人机系统的设计
4. Design of a Lift-propulsion VTOL UAV system [C] . Xin Zhao, Zhou Zhou, Xiaoping Zhu IEEE International Conference on Mechatronics and Automation . 2018

机译：升降推进VTOL UAV系统的设计
5. Control of an unconventional double-ducted fan VTOL UAV for obstructed environments using the MARC system. [D] . Dhaliwal, Sundeep S. 2009

机译：使用MARC系统控制受阻环境的非常规双导管风扇VTOL UAV。
6. Leader-Following Consensus and Formation Control of VTOL-UAVs with Event-Triggered Communications [O] . J. Fermi Guerrero-Castellanos, Argel Vega-Alonzo, Sylvain Durand, 2019

机译：领导者遵循vtol-uavs的共识和形成控制与事件触发的通信
7. Systematic design methodology for development and flight testing of a variable pitch quadrotor biplane VTOL UAV for payload delivery [O] . Chipade, Vishnu S., Abhishek, Kothari, Mangal, 2018

机译：用于开发和飞行测试的系统设计方法用于有效载荷输送的可变螺距四旋翼双翼飞机VTOL无人机
8. Tipjet VTOL UAV (Vertical Takeoff and Landing/Unmanned Aerial Vehicle) Summary. Volume 1. 1200-Pound Tipjet VTOL Unmanned Aerial Vehicle. Part 1. Conceptual Design Study of a 1200-Pound Vehicle [R] . Reader, K. R., Abramson, J. S., Schwartz, A. W., 1989

机译：Tipjet VTOL无人机（垂直起飞和着陆/无人驾驶飞行器）摘要。第1卷1200磅Tipjet VTOL无人机。第1部分：1200磅重的车辆的概念设计研究

Design of a Lift-propulsion VTOL UAV system

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