UAV Attitude Angle Measurement Method Based on Magnetometer-Satellite Positioning System

被引:0
|
作者
Qu, Gaomin [1 ,2 ]
Zhou, Zhou [1 ]
Li, Jiguang [2 ]
Shao, Zhuang [1 ]
Dong, Yanfei [2 ]
Guo, An [1 ]
机构
[1] Northwestern Polytech Univ, Sch Aeronaut, Xian 710072, Peoples R China
[2] Aircraft Acad, Xian Aeronaut Inst, Xian 710077, Peoples R China
来源
APPLIED SCIENCES-BASEL | 2022年 / 12卷 / 12期
关键词
UAV attitude angle measurement; least squares algorithm; compensation algorithm; current" statistical model; continuous-discrete Kalman filter;
D O I
10.3390/app12125947
中图分类号
O6 [化学];
学科分类号
0703 ;
摘要
Featured Application Authors are encouraged to provide a concise description of the specific application or a potential application of the work. This section is not mandatory. To improve the measurement accuracy of unmanned aerial vehicles (UAVs), in this study, we proposed a method for measuring the attitude angle of a UAV by the combination of a magnetometer and satellite positioning system. Based on the measurement principle, we established a combined measurement error model, analyzed the root cause of the measurement error, and calibrated the magnetometer using the least-squares algorithm. For handling external or system interference effects, we designed a compensation algorithm that does not depend on environmental information. For handling measurement errors, a "current" statistical model was established, and the continuous-discrete Kalman filter algorithm was used to eliminate measurement errors. The test results showed that after using the compensation algorithm, the measurement error was reduced from 17.80% to 6.86% compared to the average absolute error of the local magnetic field intensity, and the absolute measurement error was reduced by 61.49%. The absolute measurement error was compared after using the compensation + filtering algorithm, and the error after compensation was further reduced by 42.36%. Hence, we proved the feasibility and effectiveness of our method.
引用
收藏
页数:18
相关论文
共 50 条
  • [1] UAV attitude angle measurement system based on machine vision
    Hu Bo
    Chen Guangxuan
    Liu Qiang
    PROCEEDINGS OF 2020 IEEE 5TH INFORMATION TECHNOLOGY AND MECHATRONICS ENGINEERING CONFERENCE (ITOEC 2020), 2020, : 1552 - 1560
  • [2] Attitude and orbit determination for small satellite using magnetometer measurement
    Wang, JQ
    Cao, XB
    Sun, ZW
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2003, 75 (03): : 241 - 246
  • [3] Vision-based UAV Positioning Method Assisted by Relative Attitude Classification
    Zhang, Sheng
    Li, Jie
    Yang, Chengwei
    Yang, Yu
    Hu, Xiaolin
    2020 5TH INTERNATIONAL CONFERENCE ON MATHEMATICS AND ARTIFICIAL INTELLIGENCE (ICMAI 2020), 2020, : 154 - 160
  • [4] Method of Attitude Estimation in Magnetometer and Accelerometer System Based on MRPs and NPUPF
    Jie, Xu
    Qing, Guo
    PROCEEDINGS OF 2012 2ND INTERNATIONAL CONFERENCE ON COMPUTER SCIENCE AND NETWORK TECHNOLOGY (ICCSNT 2012), 2012, : 1461 - 1466
  • [5] A Noise Suppression Method in Attitude Measurement Using Global Positioning System
    Wang Bo
    Deng Zhihong
    Wang Shunting
    Fu Mengyin
    PROCEEDINGS OF THE 29TH CHINESE CONTROL CONFERENCE, 2010, : 5434 - 5437
  • [6] Reference measurement system for dynamic satellite based positioning experiments
    Däubler, L
    Filova, B
    Schrom, H
    TECHNISCHES MESSEN, 2002, 69 (03): : 125 - 130
  • [7] Strapdown gyroscope/magnetometer attitude measurement method for spinning missile
    Dai, Gang
    Li, Mei
    Su, Wei
    Shao, Bei-Bei
    Zhongguo Guanxing Jishu Xuebao/Journal of Chinese Inertial Technology, 2010, 18 (06): : 702 - 705
  • [8] Application of MIMU/Magnetometer Integrated System on the attitude determination of micro satellite
    Su, K
    Ren, DH
    You, Z
    Zhou, Q
    PROCEEDINGS OF THE 2004 INTERNATIONAL CONFERENCE ON INTELLIGENT MECHATRONICS AND AUTOMATION, 2004, : 579 - 583
  • [9] Attitude angle measurement method based on the three-dimensional accelerometer
    Tang Yufa
    Zhang He
    Hong Li
    MEASUREMENT TECHNOLOGY AND ENGINEERING RESEARCHES IN INDUSTRY, PTS 1-3, 2013, 333-335 : 152 - 156
  • [10] Attitude Determination of Nano Satellite Based on Gyroscope, Sun Sensor and Magnetometer
    Ni, Shaobo
    Zhang, Cui
    CEIS 2011, 2011, 15