Study of sensor fusion for attitude control of a quad-rotor

被引:0
|
作者
Yu, Dong-Hyeon [1 ]
Lim, Dae Young [1 ]
Sel, Nam O. [2 ]
Park, Jong Ho [2 ]
Chong, Kil To [1 ,3 ]
机构
[1] School of Department of Electronic Engineering, Chon-buk National University, Korea, Republic of
[2] School of Department of Electronic and Electronic Engineering, Seonam University, Korea, Republic of
[3] Advanced Electronics and Information Research Center, Chon-buk National University, Korea, Republic of
关键词
Kalman filters;
D O I
10.5302/J.ICROS.2015.14.8040
中图分类号
学科分类号
摘要
We presented a quad-rotor controlling algorithm design by using sensor fusion in this paper. The controller design technique was performed by a PD controller with a Kalman filter and compensation algorithm for increasing the stability and reliability of the quad-rotor attitude. In this paper, we propose an attitude estimation algorithm for quad-rotor based sensor fusion by using the Kalman filter. For this reason, firstly, we studied the platform configuration and principle of the quad-rotor. Secondly, the bias errors of a gyro sensor, acceleration and geomagnetic sensor are compensated. The measured values of each sensor are then fused via a Kalman filter. Finally, the performance of the proposed algorithm is evaluated through experimental data of attitude estimation. As a result, the proposed sensor fusion algorithm showed superior attitude estimation performance, and also proved that robust attitude estimation is possible even in disturbance. © ICROS 2015.
引用
收藏
页码:453 / 458
相关论文
共 50 条
  • [41] Gain scheduling PID Control of the Quad-rotor Helicopter
    Qiao, Jing
    Liu, Zhixiang
    Zhang, Youmin
    PROCEEDINGS OF 2017 IEEE INTERNATIONAL CONFERENCE ON UNMANNED SYSTEMS (ICUS), 2017, : 594 - 601
  • [42] Formation control of quad-rotor UAV via PIO
    Bai TingTing
    Wang DaoBo
    Masood, Rana Javed
    SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2022, 65 (02) : 432 - 439
  • [43] Formation control of quad-rotor UAV via PIO
    BAI TingTing
    WANG DaoBo
    MASOOD Rana Javed
    Science China Technological Sciences, 2022, (02) : 432 - 439
  • [44] CONTROL CHARACTERISTICS OF A BUOYANT QUAD-ROTOR RESEARCH AIRCRAFT
    NAGABHUSHAN, BL
    LICHTY, DW
    TOMLINSON, NP
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1983, 6 (02) : 91 - 99
  • [45] Active Fault Tolerant Control for a Quad-Rotor in case of a Rotor Failure
    Falcon, Romeo
    Rios, Hector
    Dzul, Alejandro
    PROCEEDINGS OF THE 2021 XXIII ROBOTICS MEXICAN CONGRESS (COMROB), 2021, : 75 - 80
  • [46] The Application of Ultrasonic Sensor in the Obstacle Avoidance of Quad-rotor UAV
    Meng Guanglei
    Pan Haibing
    2016 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2016, : 976 - 981
  • [47] Formation control of quad-rotor UAV via PIO
    TingTing Bai
    DaoBo Wang
    Rana Javed Masood
    Science China Technological Sciences, 2022, 65 : 432 - 439
  • [48] MODELING AND CONTROL OF QUAD-ROTOR DIRECTIONAL STEERING SYSTEM
    Talib, Mohammad
    Elshafei, Moustafa
    Khoukhi, Amar
    Saif, Abdul-Wahid A.
    Abdulazeez, A.
    2014 IEEE INTERNATIONAL SYMPOSIUM ON INNOVATIONS IN INTELLIGENT SYSTEMS AND APPLICATIONS (INISTA 2014), 2014, : 76 - 83
  • [49] Control system design of a quad-rotor with collision detection
    Budiyono, Agus
    Lee, Gigun
    Kim, Gyou Beom
    Park, Jungkeun
    Kang, Taesam
    Yoon, Kwang Joon
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2015, 87 (01): : 59 - 66
  • [50] MODELING, CONTROL AND NAVIGATION OF AN AUTONOMOUS QUAD-ROTOR HELICOPTER
    Sostaric, Damir
    INTERDISCIPLINARY DESCRIPTION OF COMPLEX SYSTEMS, 2016, 14 (03) : 322 - 330