小型四旋翼飞行器试验平台设计  

Design of Test Platform for Small Scale Quadrotors

作　　者：韩志凤[1] 李荣冰[1] 刘建业[1] 杭义军[1] 

机构地区：[1]南京航空航天大学自动化学院,江苏南京210016

出　　处：《测控技术》2013年第10期121-124,共4页Measurement & Control Technology

基　　金：国家自然科学基金资助项目(60904091;61104188)

摘　　要：为了实现小型四旋翼飞行器的自主导航,进行自主飞行的相关试验,并为控制器设计和微小型导航系统性能试验等研究工作提供实体验证平台,开展了小型四旋翼飞行器系统的设计。完成了系统的模块化设计,进行硬件电路设计和调试以及平台的搭建,实现导航、控制、通信等功能模块的集成。设计PC机监控软件,完成了基于USB HID协议的操纵杆数据读取,对操纵杆遥控控制模式下小型四旋翼飞行器进行实时监测,实现人机交互、控制方式选择、对飞行姿态和路线的设置、飞行器导航参数的显示等功能,开展了飞行试验,验证所设计平台各功能模块的可行性。In order to realize the independent navigation and autonomous flying on small scale quadrotors, a small quadrotor aircraft platform is designed. It can also be used as entity verification platform for the design of flight controller and performance test of micro navigation system. The vehicle system is designed, including de- sign of the hardware circuit and building of the platform. The navigation, control, communication and other function modules are integrated. In addition, a PC software is designed to monitor the status of small scale quadrotor. Reading of data, human-machine interaction, setting of the flight attitude and display of the vehicle＇ s status are realized. The flight experiment proves that each module of the small scale quadrotor is feasible.

关 键 词：四旋翼飞行器 试验平台 自主飞行 飞控系统 PC机监控软件 

分 类 号：V22[航空宇航科学与技术—飞行器设计]