A Nonlinear Attitude Estimator for Attitude and Heading Reference Systems Based on MEMS Sensors

被引:0
|
作者
Wang, Yunlong [1 ]
Soltani, Mohsen [1 ]
Hussain, Dil Muhammad Akbar [1 ]
机构
[1] Aalborg Univ, Dept Energy Technol, Esbjerg, Denmark
关键词
Nonlinear estimator; attitude estimation; MEMS sensor; OBSERVER; GYRO;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this paper, a nonlinear attitude estimator is designed for an Attitude Heading and Reference System (AHRS) based on Micro Electro-Mechanical Systems (MEMS) sensors. The design process of the attitude estimator is stated with detail, and the equilibrium point of the estimator error model is proved to be asymptotically stable using LaSalle's invariance set theorem through limitation of the range of scalar element of quaternion without affecting practical use. Also, a new Lyapunov candidate function, satisfying continuously differentiable positive definite requirement, is presented to avoid the problems in previous research works. Moreover, the estimation of MEMS gyroscope bias is also inclueded in this estimator. The designed nonlinear attitude estimator is firstly tested in simulation environment and then implemented in an AHRS hardware for further experiments. Finally, the attitude estimation results from the designed AHRS are compared with a high-precision commercial AHRS to validate its estimation performance.
引用
收藏
页码:23 / 30
页数:8
相关论文
共 50 条
  • [21] Design and implementation of a low-cost attitude and heading nonlinear estimator
    Martin, Philippe
    Salauen, Erwan
    ICINCO 2008: PROCEEDINGS OF THE FIFTH INTERNATIONAL CONFERENCE ON INFORMATICS IN CONTROL, AUTOMATION AND ROBOTICS, VOL SPSMC: SIGNAL PROCESSING, SYSTEMS MODELING AND CONTROL, 2008, : 53 - 61
  • [22] GNSS-Based Dual-Antenna Heading Augmentation for Attitude and Heading Reference Systems
    Schnaufer, Bernard
    McGraw, Gary
    Phan, Huan
    Joseph, Angelo
    PROCEEDINGS OF THE 29TH INTERNATIONAL TECHNICAL MEETING OF THE SATELLITE DIVISION OF THE INSTITUTE OF NAVIGATION (ION GNSS+ 2016), 2016, : 3669 - 3690
  • [23] 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.
    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
  • [24] Gain-Scheduled Complementary Filter Design for a MEMS Based Attitude and Heading Reference System
    Yoo, Tae Suk
    Hong, Sung Kyung
    Yoon, Hyok Min
    Park, Sungsu
    SENSORS, 2011, 11 (04) : 3816 - 3830
  • [25] Effective Adaptive Kalman Filter for MEMS-IMU/Magnetometers Integrated Attitude and Heading Reference Systems
    Li, Wei
    Wang, Jinling
    JOURNAL OF NAVIGATION, 2013, 66 (01): : 99 - 113
  • [26] Research on attitude updating algorithm based on dual quaternion for attitude and heading reference system
    Xia, Lin-Lin
    Zhao, Lin
    Liu, Fan-Ming
    Hu, Xiao-Xing
    Xitong Fangzhen Xuebao / Journal of System Simulation, 2008, 20 (02): : 276 - 280
  • [27] Survey on Attitude and Heading Reference Systems for Remotely Piloted Aircraft Systems
    Cordero, Miguel
    Alarcon, Francisco
    Jimenez, Antonio
    Viguria, Antidio
    Ollero, Anibal
    2014 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS (ICUAS), 2014, : 876 - 884
  • [28] Software algorithms in air data attitude heading reference systems
    Greene, ME
    Trent, V
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2003, 75 (05): : 470 - 476
  • [29] Testing of the attitude and heading reference system
    Tomczyk, A
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2002, 74 (02): : 154 - 160
  • [30] Automated Tuning of the Nonlinear Complementary Filter for an Attitude Heading Reference Observer
    De Silva, Oscar
    Mann, George K. I.
    Gosine, Raymond G.
    2013 IEEE WORKSHOP ON ROBOT VISION (WORV), 2013, : 171 - 176