摘要
针对当前多旋翼无人机的广泛使用以及GPS导航技术的日益成熟,使得GPS在小型飞行器上的应用成为了可能。该文研究了以APM自驾仪为核心的四轴飞行器导航系统的动力学建模原理,建立起了串级PD控制动态模型,通过MATLAB/Simulink仿真后可以得到四旋翼无人机的稳定运行效果。最后对无人机进行了航迹规划,通过实验结果证明了串级PD算法能较好地改善四旋翼无人机搭载GPS时的飞行效果。
In view of the current widespread use of multi-rotor UAVs and the increasing maturity of GPS navigation technology,which makes it possible to apply the GPS in small aircrafts.This paper studies the dynamic modeling principle of the four-axis aircraft navigation system with the APM autopilot as the core,and establishes the cascade PD control dynamic model.After the MATLAB/Simulink simulation was established,the stable operation effect of the four-axis aircraft could be obtained.Finally,the trajectory-planning of UAV was carried out,and the experimental results proved that the cascade PD algorithm can improve the flight effect of the quadcopter when equipped with GPS.
作者
杨帆
龙坤
YANG Fan;LONG Kun(School of Electrical and Information Engineering,Wuhan Institute of Technology,Wuhan 430205,China;Hubei Video Image and High-Definition Projection Engineering Technology Research Center,Wuhan 430205,China)
出处
《自动化与仪表》
2021年第8期92-97,108,共7页
Automation & Instrumentation