中图分类号： TN955+.1；TP273+.5 文献标识码： A DOI：10.16157/j.issn.0258-7998.200206 中文引用格式： 谢檬，张安莉，高原. 四旋翼无人机虚拟控制系统的设计[J].电子技术应用，2020，46(12)：67-71. 英文引用格式： Xie Meng，Zhang Anli，Gao Yuan. Design of the control system of the four-rotor UAV based on LabVIEW[J]. Application of Electronic Technique，2020，46(12)：67-71.
Design of the control system of the four-rotor UAV based on LabVIEW
Xie Meng，Zhang Anli，Gao Yuan
Xi′an Jiaotong University City College，Xi′an 710018，China
Abstract： In this paper, according to the research of four-rotor UAV control system, LabVIEW software is designed to build the data acquisition panel and query playback panel of the control system.The flight attitude parameters of the four-rotor UAV are collected in real time by the control system. The real-time data of flight altitude, flight speed, pitch angle and rolling angle are displayed in the data acquisition subpanel, and the functions of data display, processing, storage and playback are realized. The system has been tested, it realizes the attitude monitoring of UAV and meets the actual needs of controlling small four-rotor UAV.
Key words : unmanned aerial vehicle；virtual instrument；control system；data collection