Three-axis attitude control of chinese cabbage harvester cutting device based on sensor fusion

被引:1
|
作者
Park Y. [1 ]
Jun J. [2 ,3 ]
Son H.I. [2 ,3 ]
机构
[1] Department of Biosystems Engineering, Gyeongsang National University
[2] Department of Rural and Biosystemss Engineering, Chonnam National University
[3] Interdisciplinary Program in IT-Bio Convergence System, Chonnam National University
关键词
Attitude control; Chinese cabbage harvester; Kalman Filter; PID control; Sensor fusion;
D O I
10.5302/J.ICROS.2021.20.0201
中图分类号
学科分类号
摘要
In Korea, Chinese cabbage harvesting is insufficiently mechanized and automated, and this task is typically carried out using manual labor. Thus, research on Chinesee cabbage harvesters is required. However, the terrain in cabbage fields is generally rough and comprises many obstacles. Consequently, problems such as overcutting, missed cutting, and side cutting occur while cutting cabbages using a cabbage harvester. Therefore, it is necessary to study the cutting mechanism of the harvester to perform accurate cutting, considering the terrain in the fields. To this end, a three-axis attitude control mechanism was designed in this study; this mechanismm controls the cutting device of the Korean cabbage harvester with three cylinders. In addition, an accelerometer, a gyro sensor, and a rotary encoder were designed for sensor fused. The cylinders were controlled such that the measured roll (ϕ) and pitch (θ) were level with the ground. In addition, the angle of the guide in the cutting device (θe), driven by grounding to the ground, was calibrated using the height data. The cylinder in the sliding (x) axis was controlled to maintain the target height. Further, a proportional-integral-derivative controller was integrated to reduce overshoot and improve stability. To assess the performancee of the algorithm, a 2:1 scaled-down model of the cutting device of the Korean cabbage harvester was produced, and the attitude control mechanism was installed on its driving platform and tested. Attitude measurement was performed using a motion capture device (OptiTrack). For quantitative evaluation, data with and without the attitude control system were compared by estimating their root mean square error (RMSE). The RMSE values for the level and height were 0.89° and 2.23 cm, respectively, for attitude control with the posture control system; however, those for attitude control without the posture control system weree 2.15° and 4.05 cm, respectively. In addition, improvements of 58% in the levell control and 45% in the height control weree observed. In further investigations, better results can be obtained using the harvester if the changes in the angle and height are higher than those obtained in this experimental environment. © ICROS 2021.
引用
收藏
页码:277 / 284
页数:7
相关论文
共 50 条
  • [31] Design and implementation of attitude control algorithm of a satellite on a three-axis gimbal simulator
    Kabganian, Mansour
    Nabipour, Mahdi
    Saberi, Farhad F.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2015, 229 (01) : 72 - 86
  • [32] ANALYSIS ON ROOT CUTTING MECHANISM OF SELF-PROPELLED CHINESE CABBAGE HARVESTER AND OPTIMISATION OF DEVICE PARAMETERS
    Zhou, Liming
    Zeng, Yifan
    Niu, Kang
    Yuan, Yanwei
    Bai, Shenghe
    Chen, Kaikang
    INMATEH-AGRICULTURAL ENGINEERING, 2023, 71 (03): : 70 - 82
  • [33] A Soft Three-Axis Tactile Sensor based on Electromagnetic Induction
    Takenawa, Satoru
    2009 IEEE INTERNATIONAL CONFERENCE ON MECHATRONICS, VOLS 1 AND 2, 2009, : 545 - 550
  • [34] Application of hybrid robust three-axis attitude control approach to overactuated spacecraft——A quaternion based model
    A.H.Mazinan
    JournalofCentralSouthUniversity, 2016, 23 (07) : 1740 - 1753
  • [35] Three-axis MEMS combined sensor for electronic stability control system
    Jeong, Heewon
    Goto, Yasushi
    Aono, Takanori
    Nakamura, Toshiaki
    Hayashi, Masahide
    ELECTRONICS AND COMMUNICATIONS IN JAPAN, 2012, 95 (07) : 49 - 57
  • [36] Application of hybrid robust three-axis attitude control approach to overactuated spacecraft—A quaternion based model
    A. H. Mazinan
    Journal of Central South University, 2016, 23 : 1740 - 1753
  • [37] Observers Based Output Feedback Design for Three-axis Magnetic Attitude Control Systems by Bounded Controls
    Jiang, Huaiyuan
    Zhou, Bin
    PROCEEDINGS OF THE 35TH CHINESE CONTROL CONFERENCE 2016, 2016, : 1583 - 1588
  • [38] High accuracy attitude testing system based on three-axis test table
    Gao, Z.-Y. (gaozy@mail.tsinghua.edu.cn), 1600, Editorial Department of Journal of Chinese Inertial Technology (21):
  • [39] Three-axis reaction wheel attitude control system for KITSAT-3 microsatellite
    Kim, BJ
    Lee, H
    Choi, SD
    SPACE TECHNOLOGY-INDUSTRIAL AND COMMERCIAL APPLICATIONS, 1996, 16 (5-6): : 291 - 296
  • [40] STUDENT NANOSATELLITE DEVELOPMENT: FROM PASSIVE STABILIZATION TO THREE-AXIS ACTIVE ATTITUDE CONTROL
    Brak, Stefan
    Amini, Rouzbeh
    Massioni, Paolo
    GUIDANCE AND CONTROL 2009, 2009, 133 : 597 - +