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基于DSP四旋翼飞行器姿态控制系统硬件设计

吕强 郭善亮 王冬来 王珂珂

计算机与数字工程2011,Vol.39Issue(7):144-146,156,4.
计算机与数字工程2011,Vol.39Issue(7):144-146,156,4.

基于DSP四旋翼飞行器姿态控制系统硬件设计

Hardware Design of Attitude Control System for Quadrotor Based on DSP

吕强 1郭善亮 1王冬来 1王珂珂1

作者信息

  • 1. 装甲兵工程学院控制工程系 北京100072
  • 折叠

摘要

Abstract

The attitude control system is the key of quadrotor, which is a six degrees of freedom and four inputs under-actuated system. The hardware of attitude control system is designed based on DSP . TMS320F28335 is used as the main processor. The ADIS16355 inertial measurement unit is adopted for attitude information detection, while the distance is estimated with the ultrasonic sensor. The indoor test results show that the hardware system is reliable and can meet require of the attitude control system.

关键词

四旋翼飞行器/姿态控制/硬件设计/DSP

Key words

quadrotor/ attitude control/ hardware design/ DSP

分类

信息技术与安全科学

引用本文复制引用

吕强,郭善亮,王冬来,王珂珂..基于DSP四旋翼飞行器姿态控制系统硬件设计[J].计算机与数字工程,2011,39(7):144-146,156,4.

计算机与数字工程

OACSTPCD

1672-9722

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