单片机与嵌入式系统应用2016，Vol.16Issue(6)：13-16,4.
基于STM32的四旋翼飞行器姿态解算的研究
Attitude Solution of Quad-rotor Aircraft Based on STM32
李文鹏 1唐海洋1
作者信息
- 1. 西安工程大学 电子信息学院，西安 710048
- 折叠
摘要
Abstract
The quad-rotor aircraft principle of attitude solution is analyzed,and the attitude determination system is proposed which con-sists of STM32F407 and inertial measurement unit(IMU).The quaternion is used to do coordinate conversion.The complementary filter data fusion is used to obtain the accurate attitude angle,and then completes the attitude calculation.The experiment results show that the filtering algorithm effectively combines the complementary sensor data of the inertial measurement unit to achieve high precision attitude calculation.关键词
四旋翼飞行器/飞行控制系统/姿态解算/互补滤波器/STM32F407Key words
quad-rotor aircraft/flight control system/attitude solution/complementary filter/STM32F407分类
信息技术与安全科学引用本文复制引用
李文鹏,唐海洋..基于STM32的四旋翼飞行器姿态解算的研究[J].单片机与嵌入式系统应用,2016,16(6):13-16,4.
