Attitude and Heading Reference System for Quadrotor Based on MEMS Sensors

被引:4
|
作者
Jiang, Qiang [1 ]
Zeng, Yong [1 ]
Liu, Qiang [1 ]
Jing, Hua [1 ]
机构
[1] UESTC, Sch Aeronaut & Astronaut, Chengdu, Peoples R China
关键词
AHRS; quaternion; Kalman; quadrotor;
D O I
10.1109/IMCCC.2012.257
中图分类号
TP301 [理论、方法];
学科分类号
081202 ;
摘要
This paper deals with designing and implementation of Attitude and Heading Reference System (AHRS) which based on data fusion of multi-sensor. And it presents an approach of designing a low cost AHRS which used Micro Electronic Mechanical System (MEMS). In our approach, AHRS is made up of a 3-axes MEMS accelerometers, a 3-axes MEMS rate-gyros, an electronic compass and a FPGA which is used as the signal processor. Furthermore, a rotation quaternion and a Kalman Filter were the options as multi-sensor data fusion and integration. Finally, an experiment was introduced to analyze the attitude data carried on quadrotor. The simulation test shows when the carrier is in dynamic environment, the attitudes error are within 2 degrees. The results show that the designed AHRS provided stabilized attitude and heading angles in dynamic conditions which improved the quadrotor's attitude and heading control.
引用
收藏
页码:1090 / 1093
页数:4
相关论文
共 50 条
  • [1] A LOW COST ATTITUDE AND HEADING REFERENCE SYSTEM BASED ON A MEMS IMU FOR A T-QUADROTOR
    Long, Yangbo
    Bai, Shi
    Patel, Paras
    Cappelleri, David J.
    [J]. PROCEEDINGS OF THE ASME INTERNATIONAL DESIGN ENGINEERING TECHNICAL CONFERENCES AND COMPUTERS AND INFORMATION IN ENGINEERING CONFERENCE - 2011, VOL 6, PTS A AND B, 2012, : 863 - 870
  • [2] A Nonlinear Attitude Estimator for Attitude and Heading Reference Systems Based on MEMS Sensors
    Wang, Yunlong
    Soltani, Mohsen
    Hussain, Dil Muhammad Akbar
    [J]. PROCEEDINGS OF 2016 SICE INTERNATIONAL SYMPOSIUM ON CONTROL SYSTEMS (ISCS 2016), 2016, : 23 - 30
  • [3] GPS Aided Attitude and Heading Reference System using MEMS Sensors
    Ailneni, Sanketh
    [J]. 2016 INDIAN CONTROL CONFERENCE (ICC), 2016, : 412 - 417
  • [4] Application of UKF for MEMS IMUs and fluxgate sensors based attitude and heading reference system of carriers
    Zhao, Lin
    Xia, Linlin
    Liu, Famning
    Cheng, Yi
    [J]. ICIEA 2007: 2ND IEEE CONFERENCE ON INDUSTRIAL ELECTRONICS AND APPLICATIONS, VOLS 1-4, PROCEEDINGS, 2007, : 2278 - 2283
  • [5] Design of Attitude and Heading Reference System Based on MEMS Sensor
    Liu, Zhiping
    Wu, Lili
    [J]. PROCEEDINGS OF THE 2012 24TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2012, : 2597 - 2601
  • [6] Implementation and Evaluation of Attitude Heading and Reference System Based on MEMS
    Liu, Zhiping
    Wang, Yawen
    [J]. PROCEEDINGS OF THE 32ND 2020 CHINESE CONTROL AND DECISION CONFERENCE (CCDC 2020), 2020, : 5404 - 5408
  • [7] Fault detection and isolation enhancement of an aircraft attitude and heading reference system based on MEMS inertial sensors
    Carminati, M.
    Ferrari, G.
    Sampietro, M.
    Grassetti, R.
    [J]. PROCEEDINGS OF THE EUROSENSORS XXIII CONFERENCE, 2009, 1 (01): : 509 - +
  • [8] Adaptive filter for a miniature MEMS based attitude and heading reference system
    王玫
    王永泉
    张炎华
    [J]. Journal of Harbin Institute of Technology(New series), 2006, (05) : 571 - 575
  • [9] Adaptive filter for a miniature MEMS based attitude and heading reference system
    Wang, M
    Yang, YC
    Hatch, RR
    Zhang, YH
    [J]. PLANS 2004: POSITION LOCATION AND NAVIGATION SYMPOSIUM, 2004, : 193 - 200
  • [10] The Design of Attitude Heading Reference System Based on MEMS Sensing Technology
    Huang, Pengge
    Lv, Haojie
    [J]. 2017 6TH DATA DRIVEN CONTROL AND LEARNING SYSTEMS (DDCLS), 2017, : 242 - 246