Electronics Optics & Control, Volume. 24, Issue 8, 9(2017)

On Attitude Estimation System of Spinning Missile Based on Solar Vector and MEMS

XU Guang-yan... LIAO Pei-chong and ZHANG Hong-mei |Show fewer author(s)
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    References(6)

    [3] [3] WANG M, YANG Y C, HATCH R R, et al.Adaptive filter for a miniature MEMS based attitude and heading refe-rence system[C]//Position Location and Navigation Symposium, 2004:193-200.

    [5] [5] 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]//Sensor, IEEE,2005.doi:10.1109/ICSENS.2005.1597968.

    [6] [6] ZHANG R H, JIA H G, CHEN T, et al.Attitude solution enginccring for strapdown inertial navigation system based on quaternion algorithm[J].Optics Precision Engineering, 2008, 16(10):1963-1970.

    [7] [7] ANGRISANO A.GNSS/INS Integration methods[D].Calgary:University of Calgary, 2010.

    [8] [8] GUERRERO-CASTELIANOS J F, MADRIGAL-SASTRE H, DURAND S, et al.Design and implementation of an attitude and heading reference system[C]//The 8th International Conference on Electrical Engineering, Computing Science and Automatic Control, Program and Abstract Book, 2011:1-5.

    [11] [11] DENTI E, GALATOLO R, SCHETTINI F.An AHRS based on a Kalman filter for the integration of intertial, magnet-ometric an GPS data[C]//The 27th Internation Congress of the Aeronautical Sciences, 2010:1-9.

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    XU Guang-yan, LIAO Pei-chong, ZHANG Hong-mei. On Attitude Estimation System of Spinning Missile Based on Solar Vector and MEMS[J]. Electronics Optics & Control, 2017, 24(8): 9

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    Paper Information

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    Received: Jun. 30, 2016

    Accepted: --

    Published Online: Sep. 21, 2017

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2017.08.003

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