中圖分類號(hào)： TN955+.1；TP273+.5 文獻(xiàn)標(biāo)識(shí)碼： A DOI：10.16157/j.issn.0258-7998.200206 中文引用格式： 謝檬，張安莉，高原. 四旋翼無人機(jī)虛擬控制系統(tǒng)的設(shè)計(jì)[J].電子技術(shù)應(yīng)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
