Orthogonal Design and Optimization of Flight Stability Test for the Quadrotor Unmanned Aerial Vehicle

被引：0
|
作者：
Hu, Xiaodong [1 ]
Huang, Xuexiang [1 ]
机构：
[1] Beijing Inst Tracking & Telecommun Technol, Beijing, Peoples R China
来源：
PROCEEDINGS OF 2017 IEEE INTERNATIONAL CONFERENCE ON UNMANNED SYSTEMS (ICUS) | 2017年
关键词：
Quadrotor UAV; Stability; Orthogonal Design; MATLAB;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The flight stability test of the quadrotor UAV (Unmanned Aerial Vehicle) is an important means to test the correctness of the design scheme of the UAV system. The paper adopts orthogonal design to study the factors that affect the flight stability of the quadrotor UAV. In this paper, several natural factors and control factors, such as wind and throttle control, are taken as the research object. The paper studies the influence of the above factors on the flight stability of the quadrotor UAV, and the algorithm is verified by MATLAB software.
引用
收藏
页码：343 / 346
页数：4
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