摘要
针对无人飞艇的架构与性能特点,设计一种基于ATmega2560微处理器和MPU6050作为惯性测量单元的无人飞艇飞行控制系统;介绍了该控制系统的总体结构以及软、硬件设计方法,包括惯性测量模块和电机驱动控制模块;并给出了该系统的设计流程图。通过搭建地面实时仿真环境,对飞艇飞行姿态、航线及反馈量等进行仿真,仿真结果表明,飞控系统处理速度快和解算精度高。经无人飞艇使用表明,该飞行控制系统设计合理,能够满足飞艇的性能要求,具有一定的工程使用价值。
In this article,a flight control system for unmanned airship based on ATmega2560 as the master chip,and MPU6050 as inertial measurement unit is developed aiming at the problem of the constitution and features of unmanned airship.The whole structure and the disigh of software and hardware are introduced in detail.Including IMU module and motor conteol module.The software flowchart is also presented.The airship flight attitude flight path and feedback volume have been simulated by building the ground real-time simulation environm ent.The simulation results have proved that the speed and accuracy of flight control system is high. This controler is verified by unmanned airship,The experiments shows that the design of the flight control system is reasonable and it satisfies the performance requirements of the unmanned airship and further engineering applications.
作者
彭平
Peng Ping(China Special Vehicle Research Institute,Jingmen 48000,China)
出处
《电子测量技术》
2019年第19期59-62,共4页
Electronic Measurement Technology