Electronics Optics & Control, Volume. 23, Issue 10, 75(2016)

Continuous Rotation Self-Alignment Technology of HRG Initial Platform

CHEN Wei... LIU Jie-yu, ZHOU Xiao-gang and SUN Tian-chuan |Show fewer author(s)
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    References(4)

    [1] [1] ROZELLE D M.The hemispherical resonator gyro:from wineglass to the planets[J].Spaceflight Mechanics, 2009, 134:1-26.

    [5] [5] BAR-ITZHACK I Y, PORAT B.Azimuth observability enhancement during inertial navigation system in-flight alignment[J].Journal of Guidance, Control, and Dyna-mics, 1980, 3(4):337-344.

    [6] [6] ANDREW D J.Continuous calibration and alignment techniques for an all-attitude inertial platform[R].Key Bis-cayne:American Institiute of Aeronautics and Astronautics, 1973.

    [9] [9] GELLER E S.Inertial system platform rotation[J].IEEE Transactions on Aerospace and Electronic Systems, 1968, 4(4):557-568.

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    CHEN Wei, LIU Jie-yu, ZHOU Xiao-gang, SUN Tian-chuan. Continuous Rotation Self-Alignment Technology of HRG Initial Platform[J]. Electronics Optics & Control, 2016, 23(10): 75

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    Paper Information

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    Received: Sep. 11, 2015

    Accepted: --

    Published Online: Nov. 18, 2016

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2016.10.016

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