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基于MEMS的微型飞行器姿态测量系统
引用本文:曹晓棠,石云波,周兆英,刘绍鹏,郭奇,赵斐.基于MEMS的微型飞行器姿态测量系统[J].传感器与微系统,2013,32(2):122-123,127.
作者姓名:曹晓棠  石云波  周兆英  刘绍鹏  郭奇  赵斐
作者单位:中北大学电子测试技术国家重点实验室,山西太原,030051
基金项目:国家自然科学基金资助项目(51075375)
摘    要:利用三轴加速度计和三轴磁强计,设计了基于MEMS技术的微型飞行器姿态测量系统。系统采用C8051F单片机进行各传感器的数据采集,通过串口通信将采集的信息发送到上位机,用四元数解算算法进行数据融合和姿态解算,将俯仰角,横滚角、航向角等信息在上位机界面上显示出来。

关 键 词:微机电系统  姿态测量  上位机

Attitude measurement system for micro air vehicle based on MEMS
CAO Xiao-tang , SHI Yun-bo , ZHOU Zhao-ying , LIU Shao-peng , GUO Qi , ZHAO Fei.Attitude measurement system for micro air vehicle based on MEMS[J].Transducer and Microsystem Technology,2013,32(2):122-123,127.
Authors:CAO Xiao-tang  SHI Yun-bo  ZHOU Zhao-ying  LIU Shao-peng  GUO Qi  ZHAO Fei
Affiliation:(National Key Laboratory of Electronic Measurement Technology,North University of China, Taiyuan 030051,China)
Abstract:Using three-axis accelerometer and three-axis magnetometer,an attitude measurement system based on MEMS for micro air vehicle is designed.The system uses C8051F MCU to collect datas of sensors,and datas are sent to upper PC by serial communication,then four element algorithm is used for data fusion and attitude calculation,the pitch,roll,heading angle is displayed on the interface of upper PC.
Keywords:MEMS  attitude measurement  upper PC
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