首页 | 本学科首页   官方微博 | 高级检索  
     检索      

无人地效飞行器控制系统研究
引用本文:李光春,李官茂,高延滨,何昆鹏,王庭军.无人地效飞行器控制系统研究[J].导航与控制,2011(3):1-5.
作者姓名:李光春  李官茂  高延滨  何昆鹏  王庭军
作者单位:哈尔滨工程大学自动化学院;哈尔滨工程大学自动化学院;哈尔滨工程大学自动化学院;哈尔滨工程大学自动化学院;哈尔滨工程大学自动化学院
摘    要:针对无人地效飞行器的特点,基于MEMS陀螺、加速度计和电子罗盘等传感器设计了飞行控制系统.详细介绍飞行器数学建模、数据融合算法以及飞行控制系统软件设计.仿真结果和实物飞行表明;该系统稳定性好、精度高,能够满足实时控制的要求.

关 键 词:无人地效飞行器  MEMS  姿态检测  飞行控制

Research on the Control System for Unmanned Ground Effect Vehicle
LI Guang-chun,LI Guan-mao,GAO Yan-bin,HE Kun-peng and WANG Ting-jun.Research on the Control System for Unmanned Ground Effect Vehicle[J].Navigation and Control,2011(3):1-5.
Authors:LI Guang-chun  LI Guan-mao  GAO Yan-bin  HE Kun-peng and WANG Ting-jun
Institution:School Of Automation, Harbin Engineering University;School Of Automation, Harbin Engineering University;School Of Automation, Harbin Engineering University;School Of Automation, Harbin Engineering University;School Of Automation, Harbin Engineering University
Abstract:According to the characteristics of unmanned ground effect vehicle, designed the flight control system. It is based on the MEMS gyroscope, accelerometer and electronic compass sensors. The introduction of mathematical modeling, data fusion algorithm of aircraft and flight control system software design is detailed. The simulation and flighting experiment proved the good stability, high accuracy and real-time of the control system.
Keywords:unmanned ground effect vehicle  MEMS  attitude measurement  flight control
点击此处可从《导航与控制》浏览原始摘要信息
点击此处可从《导航与控制》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号