• Electronics Optics & Control
  • Vol. 23, Issue 10, 75 (2016)
CHEN Wei, LIU Jie-yu, ZHOU Xiao-gang, and SUN Tian-chuan
Author Affiliations
  • [in Chinese]
  • show less
    DOI: 10.3969/j.issn.1671-637x.2016.10.016 Cite this Article
    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 Copy Citation Text show less
    References

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

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

    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
    Download Citation