Modeling and Simulation of a Propeller-Engine System for Unmanned Aerial Vehicles

被引：0

作者：

Martinez-Alvarado, R. ^{[1
]}

Granda-Gutierrez, E. E. ^{[1
]}

Sanchez-Orta, A. ^{[2
]}

Ruiz-Sanchez, F. J. ^{[2
]}

机构：

[1] COMIMSA, Adv Mfg Postgrad Program, Saltillo, Coahuila, Mexico

[2] CINVESTAV, Robot & Adv Mfg Grp, Saltillo, Coahuila, Mexico

来源：

2013 IEEE INTERNATIONAL AUTUMN MEETING ON POWER, ELECTRONICS AND COMPUTING (ROPEC) | 2013年

关键词：

Modeling of Brushless Direct Current; Thruster; Aerodynamic Load torque; UAV Control; MOTORS;

D O I：

暂无

中图分类号：

TE [石油、天然气工业]; TK [能源与动力工程];

学科分类号：

0807 ; 0820 ;

摘要：

In this paper we present a model of a Propeller-Engine system and a simulation analysis of its dynamics in order to estimate the total load torque produced by the aerodynamic effects of a spinning propeller attached to its rotor when it is used as a thruster in small scale Unmanned Aerial Vehicles. The contribution is twofold: first, we obtain the model of a composed propeller-engine system introducing the mechanical load of a turning propeller to the electro-mechanical properties of a Brushless Direct Current motor, to determine the total thrust and the load torque with respect to its angular velocity, and then, we present the results of a numerical simulation of its dynamical behavior under hovering conditions. The aim of this work is to establish the basis for new developments in the area of control to improve the stability of flight in Unmanned Aerial Vehicles avoiding drifting.

引用

页数：6

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