Circuit Design of the Flight Attitude Control System for a Quadrotor Unmanned Aerial Vehicle
谢轩XIE Xuan;谢完成XIE Wan-cheng
（娄底职业技术学院,娄底417000 )
( Loudi Vocational and 'Technical College , Loudi 417000, China )
摘要:近年来四旋翼无人机因其自身的特点已经被应用到各个领域,无人机飞行的稳定性直接影响到它的生存能力,因此，飞行姿态控制系统电路设计引起了研究人员的高度重视。飞行控制系统电路中元器件参数的选择对无人机的飞行姿态控制有着至关重要的作用。本文以STM32微控制器为核心,利用MPU9250作为采集四旋翼无人机姿态数据传感器,基于模糊PID控制算法,实现四旋翼无人机飞行姿态控制系统电路设计。
Abstract: In recent years, quadcopter drones have been applied in various fields due to their own characteristics. The stability of droneflight directly affects its survival ability. Therefore,the circuit design of flight attitude control system has atracted high attention fromresearchers. The selection of component parameters in the flight control system circuit plays a crucial tole in the flight attitude control ofunmanned aerial vehicles.'This article takes the STM32 microcontroller as the core, uses MPU9250 as the sensor to collect the attitude dataof a (quadcopter unmanned aerial vehicle,and implements the circuit design of the flight attitude control system for the quadcoplerunmanned aerial vehicle based on the fuzzy PID control algorithm.
关键词:四旋翼无人机;姿态控制;电路设计
Key words: quadcopter drone; attitude control; circuit design
价值工程-文章出处：谢轩,谢完成.四旋翼无人机飞行姿态控制系统电路设计[J].价值工程,2023,42(20):73-75. |
