宇航计测技术

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四轴飞行器姿态监控系统设计

王金红1,2；成怡1,2；钱红亮1,2；谢飞1,2   

  1. 1、天津工业大学 电气工程与自动化学院，天津 300387；
    2、天津工业大学 电工电能新技术天津市重点实验室，天津 300387
  • 出版日期:2014-12-15 发布日期:2014-12-15
  • 作者简介:王金红（1989-），女，硕士研究生，主要研究方向：控制科学与工程、惯性导航技术的研究。

Design of Four Axis Aircraft Attitude Control System

WANG Jin-hong1,2；CHENG Yi1,2；QIAN Hong-liang1,2；XIE Fei1,2   

  1. 1、School of Electrical Engineering and Automation，Tianjin Polytechnic University，Tianjin 300387；
    2.、Electrical power Tianjin Key Laboratory of new technology，Tianjin Polytechnic University，Tianjin 300387
  • Online:2014-12-15 Published:2014-12-15

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摘要： 设计了一套四轴飞行器上位机监控系统。针对准确掌握四轴飞行器的实时姿态、位置等信息和对四轴飞行器进行精准控制两大核心问题，开发了由上位机实现四轴飞行器姿态数据采集、通信及控制等功能的监控系统。监控系统良好的功能设计和友好的人机界面使得用户能够准确掌握飞行器的飞行信息，从而能够更精准地控制四轴飞行器飞行姿态。实验验证，监控系统简单实用，性能稳定，精度高，使整个飞行系统抗干扰能力强，鲁棒性、稳定性好。

关键词: 四轴飞行器, 姿态数据, 上位机, 监控系统, 控制界面

Abstract: A set of four axis aircraft PC monitoring system is designed. To accurately grasp the real-time attitude, position information of the four axis aircraft and to precisely control the four axis aircraft, the monitoring system is developed by the host computer to realize four axis aircraft attitude data acquisition, communication and control functions. The function design of the control system is good and friendly man-machine interface enables the user to accurately grasp the flight information of four axis aircraft flight. So four axis aircraft is controlled more accurately. Experimental verification, the monitoring system is simple and practical, stable performance, high precision, which makes the anti-interference ability of control system stronger, maintains better robustness and stability.

Key words: Four axis aircraft, Attitude data, Host computer, Monitoring system, Control interface

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