摘要
本文以南航研究成功的某型号微型飞行器为背景,用理论计算和试验验证的方法,研究了利用传统飞行器飞行力学方程推算微型飞行器驱动装置参数的可行性,同时研究了静态条件下电动机和螺旋桨的不同匹配对整个动力装置的影响。
In this paper the feasibility of calculating the parameters of MAV＇ s drive by employing the traditional flight dynamic equations is studied based on a successful MAV of NUAA by theory computation combined with test validation. The influence of different motor-propeller matching on the drive device is also studied in static conditions.
出处
《科技广场》
2006年第7期4-6,共3页
Science Mosaic
关键词
微型飞行器
电动机
工作特性
螺旋桨
Micro Air Vehicle
Motor
Operating Characteristics
Propeller
