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

doi:10.13873/j.1000-97872013.02.012

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Attitude measurement system for micro air vehicle based on MEMS

更新时间：2025-09-11

- Attitude measurement system for micro air vehicle based on MEMS
- Vol. 32, Issue 2, Pages: 122-123+127(2013)
- 作者机构：
  
  中北大学电子测试技术国家重点实验室
- 作者简介：
- 基金信息：
- DOI：10.13873/j.1000-97872013.02.012
  CLC： V556
- Published：2013
- 稿件说明：
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[1]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(02):122-123+127.

CAO Xiao-tang, SHI Yun-bo, ZHOU Zhao-ying, et al. Attitude measurement system for micro air vehicle based on MEMS[J]. 2013, 32(2): 122-123+127.
[1]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(02):122-123+127. DOI： 10.13873/j.1000-97872013.02.012.

CAO Xiao-tang, SHI Yun-bo, ZHOU Zhao-ying, et al. Attitude measurement system for micro air vehicle based on MEMS[J]. 2013, 32(2): 122-123+127. DOI： 10.13873/j.1000-97872013.02.012.

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。

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.

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references

基于MEMS压力传感器的微小型空速计 [J]. 王立代,熊沈蜀,周兆英. 清华大学学报(自然科学版) . 2005(08)

小型无人机飞行控制器的硬件设计 [J]. 刘歌群. 计算机测量与控制 . 2003(02)

数字式无人机飞行控制系统研制 [J]. 袁锁中. 计算机测量与控制 . 2003(01)

Kalman滤波理论及其在导航系统中的应用[M]. 科学出版社 , 付梦印等编著, 2003

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