四旋翼无人机飞行姿态控制系统电路设计  

Circuit Design of the Flight Attitude Control System for a Quadrotor Unmanned Aerial Vehicle

作　　者：谢轩[1] 谢完成[1] XIE Xuan;XIE Wan-cheng(Loudi Vocational and Technical College,Loudi 417000,China)

机构地区：[1]娄底职业技术学院,娄底417000

出　　处：《价值工程》2023年第20期73-75,共3页Value Engineering

基　　金：2022年湖南省教育厅科学研究项目“基于深度学习的植保无人机监测系统研究”(立项编号:22C1264)。

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。In recent years,quadcopter drones have been applied in various fields due to their own characteristics.The stability of drone flight directly affects its survival ability.Therefore,the circuit design of flight attitude control system has attracted high attention from researchers.The selection of component parameters in the flight control system circuit plays a crucial role in the flight attitude control of unmanned aerial vehicles.This article takes the STM32 microcontroller as the core,uses MPU9250 as the sensor to collect the attitude data of a quadcopter unmanned aerial vehicle,and implements the circuit design of the flight attitude control system for the quadcopter unmanned 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 

分 类 号：V279[航空宇航科学与技术—飞行器设计]