| 注册
首页|期刊导航|现代电子技术|某后推式全动平尾电动手抛无人机的定高控制设计

某后推式全动平尾电动手抛无人机的定高控制设计

马云飞 朱菲菲

现代电子技术Issue(13):13-15,20,4.
现代电子技术Issue(13):13-15,20,4.

某后推式全动平尾电动手抛无人机的定高控制设计

Design for fixed altitude control of UAV with pushback stabilator and electric hand-fling

马云飞 1朱菲菲1

作者信息

  • 1. 中国电子科技集团公司 第二十七研究所,河南 郑州 450047
  • 折叠

摘要

Abstract

UAV fixed altitude fight control technology with pushback stabilator and electric hand⁃fling is studied. UAV flight control rules were designed according to flight control system theory. Then on the basis of it,UAV longitudinal control rules were designed by using classic PID control. Since the large disturbance is generated when the altitude is changeable with accelerator in actual flight,the method which adopts altitude⁃accelerator control loop to compensate longitudinal control is pro⁃posed to improve UAV altitude control precision. The actual flight verification is conducted on a small electric hand⁃fling UAV. Flight results show that the altitude control method is reasonable and effective,and it has extensive reference significance.

关键词

无人机/电动/定高/高度控制

Key words

UAV/electric driven/fixed altitude/altitude control

分类

信息技术与安全科学

引用本文复制引用

马云飞,朱菲菲..某后推式全动平尾电动手抛无人机的定高控制设计[J].现代电子技术,2015,(13):13-15,20,4.

现代电子技术

OA北大核心CSTPCD

1004-373X

访问量0
|
下载量0
段落导航相关论文