Take-off and landing control for a coaxial ducted fan unmanned helicopter

Chen Zhi; Wang Daobo; Zhen Ziyang; Wang Biao; Fu Jian

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Take-off and landing control for a coaxial ducted fan unmanned helicopter

机译：同轴管道风扇无人直升机的起降控制

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摘要

Purpose - This paper aims to present a control strategy that eliminates the longitudinal and lateral drifting movements of the coaxial ducted fan unmanned helicopter (UH) during autonomous take-off and landing and reduce the coupling characteristics between channels of the coaxial UH for its special model structure.

机译：目的-本文旨在提出一种控制策略，以消除同轴风管无人直升机（UH）在自主起飞和着陆期间的纵向和横向漂移运动，并针对其特殊型号降低同轴UH通道之间的耦合特性结构体。

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来源
《Aircraft engineering》 |2017年第6期|764-776|共13页
作者
Chen Zhi; Wang Daobo; Zhen Ziyang; Wang Biao; Fu Jian;
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作者单位

Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing, Jiangsu, Peoples R China;

Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing, Jiangsu, Peoples R China;

Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing, Jiangsu, Peoples R China;

Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing, Jiangsu, Peoples R China;

Nanjing Univ Aeronaut & Astronaut, Sch Energy & Power Engn, Nanjing, Jiangsu, Peoples R China;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类
关键词
Coupling characteristics; Drifting movement; Quick flight trim; Take-off and landing; Terminal sliding mode control (TSMC); Unmanned helicopter (UH);

机译：耦合特性;漂移运动;快速飞行调整;起降;终端滑模控制（TSMC）;无人直升机（UH）;

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专利

1. Modeling and Sliding Mode Control with Boundary Layer for Unmanned Coaxial Rotor Ducted Fan Helicopter [J] . Chen Zhi, Wang Daobo, Zeng Ziyang, 南京航空航天大学学报（英文版） . 2016,第002期

机译：无人同轴转子风管直升机的边界层建模与滑模控制
2. Simulation and analysis of flow around tilting asymmetric ducted fans mounted at the wing tips of a vertical take-off and landing unmanned aerial vehicle [J] . Raeisi Bahram, Alighanbari Hekmat Proceedings of the Institution of Mechanical Engineers . 2018,第15期

机译：模拟和分析安装在垂直起降无人机翼尖上的不对称倾斜管道风机周围的流动
3. Effects of tilting rate variations on the aerodynamics of the tilting ducted fans mounted at the wing tips of a vertical take-off and landing unmanned aerial vehicle [J] . Raeisi Bahram, Alighanbari Hekmat Proceedings of the Institution of Mechanical Engineers . 2018,第10期

机译：倾斜速率变化对安装在垂直起降无人飞行器机翼尖端的倾斜式管道风扇空气动力学的影响
4. Longitudinal and lateral adaptive flight control design for an unmanned helicopter with coaxial rotor and ducted fan [C] . Sheng Shouzhao, Sun Chenwu, Duan Haibin, Chinese Control Conference . 2014

机译：带有同轴转子和管道风扇的无人直升机的纵向和横向自适应飞行控制设计
5. Design of an automatic landing system for twin rotor vertical take-off and landing unmanned air vehicle. [D] . Bole, Michael. 2000

机译：双转子垂直起降无人飞行器自动着陆系统的设计。
6. Control System for Vertical Take-Off and Landing Vehicle’s Adaptive Landing Based on Multi-Sensor Data Fusion [O] . Hongyan Tang, Dan Zhang, Zhongxue Gan 2020

机译：基于多传感器数据融合的垂直起飞和着陆车辆自适应降落控制系统
7. Simulation Environment for Development of Unmanned Helicopter Automatic Take-off and Landing on Ship Deck [O] . Antonio Vitale, Davide Bianco, Gianluca Corraro, 2018

机译：无人驾驶直升机自动起飞和船甲板降落的仿真环境

Take-off and landing control for a coaxial ducted fan unmanned helicopter

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