Optimizing Performance Variables for Small Unmanned Aerial Vehicle Co-axial Rotor Systems

被引：0

作者：

Bell, Jonathon ^{[1
]}

Brazinskas, Mantas ^{[1
]}

Prior, Stephen ^{[1
]}

机构：

[1] Middlesex Univ, Sch Engn & Informat Sci, London N14 4YZ, England

来源：

ENGINEERING PSYCHOLOGY AND COGNITIVE ERGONOMICS | 2011年 / 6781卷

关键词：

Co-axial Rotor; SUAV; Aerodynamics; H/D ratio;

D O I：

暂无

中图分类号：

TP18 [人工智能理论];

学科分类号：

081104 ; 0812 ; 0835 ; 1405 ;

摘要：

The aim of this project was to design and build a test-rig that is capable of analyzing small unmanned aerial vehicles (SUAV) co-axial rotor systems. The intention of the test-rig development was to highlight important aeromechanical components and variables that dictate the co-axial units flight performance, with the intention of optimizing the propulsion systems for use on HALO (R) a co-axial SUAV designed by the Autonomous Systems Lab at Middlesex University. The major contributions of this paper are: an optimum COTS co-axial configuration with regards to motor and propeller variations, a thorough review and validation of co-axial rotor systems inter-rotor spacing which in turn identified an optimum H/D ratio region of between (0.41-0.65).

引用

页码：494 / 503

页数：10

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