Optics and Precision Engineering, Volume. 22, Issue 12, 3280(2014)

Attitude estimation base on gravity/magnetic assisted Euler angle UKF

JIA Rui-cai*
Author Affiliations
  • [in Chinese]
  • show less
    References(17)

    [3] [3] WANG M,YANG Y C, HATCH R R. Adaptive filter for a miniature MEMS based attitude and heading reference system[C]. Position Location and Navigation Symposium, 2004.

    [4] [4] EGZIABHER D G, HAYWARD R C, POWELL J D. Design of multisensory attitude determination systems[J]. Aerospace and Electronic Systems, IEEE Transactions, 2004, 40(2): 627- 649.

    [5] [5] YANG Y, FARRELL J A. Two antennas GPS-aided INS for attitude determination[C]. IEEE Transactions on Control Systems Technology, 2003.

    [6] [6] CASTELLANOS J F G, LESECQ S, MARCHAND N, et al.. A low cost air data attitude heading reference system for the tourism airplane applications [C]. Sensors, IEEE, 2005.

    [7] [7] ZHANG R H, JIA H G, CHEN T, et al.. Attitude solution for strapdown inertial navigation system based on quaternion algorithm [J].Opt. Precision Eng., 2008,16(10): 1963-1970. (in Chinese)

    [8] [8] ANGRISANO A. GNSS/INS Integration Methods[D]. Canada: University of Calcary,2010.

    [9] [9] GUERRERO C J F. Design and implementation of an attitude and heading reference system[C]. 8th International Conference on Electrical Engineering, Computing Science and Automatic Control, Program and Abstract Book, 2011.

    [10] [10] GAO Z Y, NIU X J, GUO M F. Quaternion-based kalman filter for micro-machined strapdown attitude heading reference system[J]. Chinese Journal of Aeronautics, 2002,15(3): 171-175.

    [11] [11] KLEIN I, FILIN S, TOLEDO T. Pseudo- measurements as aiding to INS during GPS outages[J]. Navigation,2010,57(1): 25-34.

    [12] [12] PAHADIA A. GPS/INS Integration Aided with Gyroscope-Free IMU for Pedestrian Applications[D]. Canada: Department of Geomatics Engineering, University of Calgary, UCGE Report, 2010.

    [13] [13] QIAO X W, ZHOU W D, JI Y R. Aircraft attitude estimation based on quaternion state-switching unscented Kalman filter [J]. Control Theory & Applications, 2012,29(1): 97-103.(in Chinese)

    [14] [14] DAH J J,TA S. Critical remarks on the linearised and extended kalman filters with geodetic navigation examples[J]. Measurement, 2010,43(9): 1077-1089.

    [15] [15] HONG H Q, MOORE J B. Direct kalamn filtering approach for GPS/INS integration. Aerospace and Electronic Systems [J].IEEE Transactions on, 2002,38(2): 687-693.

    [16] [16] EL-SHEIMY N. Inertial techniques and INS/DGPS Integration[D]. Canada: Department of Geomatics Engineering, University of Calgary, 2004.

    [17] [17] GEBRE D, ELKAIM G H, POWELL J D, et al.. A gyro-free quaternion-based attitude determination system suitable for implementation using low cost sensors[C]. Position Location and Navigation Symposium, IEEE 2000.

    CLP Journals

    [1] LI Zhao-ming, YANG Wen-ge, DING Dan, LIAO Yu-rong. Fifth-degree strong tracking cubature Kalman filter for real-time orbit determination by multiple terminals[J]. Optics and Precision Engineering, 2017, 25(8): 2195

    [2] LI Zeng-yan, LI Xiao-min, LIU Qiu-sheng, ZHOU Zhao-ying. Adaptive fast initial attitude estimation for inflight loitering munition[J]. Optics and Precision Engineering, 2017, 25(2): 493

    Tools

    Get Citation

    Copy Citation Text

    JIA Rui-cai. Attitude estimation base on gravity/magnetic assisted Euler angle UKF[J]. Optics and Precision Engineering, 2014, 22(12): 3280

    Download Citation

    EndNote(RIS)BibTexPlain Text
    Save article for my favorites
    Paper Information

    Category:

    Received: Mar. 9, 2014

    Accepted: --

    Published Online: Jan. 13, 2015

    The Author Email: Rui-cai JIA (jiaruicai@126.com)

    DOI:10.3788/ope.20142212.3280

    Topics