• Electronics Optics & Control
  • Vol. 21, Issue 7, 95 (2014)
HOU Yu-hong and LIANG Bao-hua
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2014.07.021 Cite this Article
    HOU Yu-hong, LIANG Bao-hua. A Method for Obtaining Navigation Sensor Flight Testing Benchmark[J]. Electronics Optics & Control, 2014, 21(7): 95 Copy Citation Text show less
    References

    [1] TIAN X M, LEI X.Usage of airborne multi-sensor data fusion technology in air battle [J].Avionics Technology, 2002, 33(1): 36-40.

    [2] QIN Y Y, ZHANG H Y, WANG S H.Theory of Kalman filter and integrated navigation [M].Xian:Northwestern Polytechnical University Press, 2004.

    [3] YANG Y J, JIN Z H, TIAN W F, et al.Application of R-T-S optimal smoothing algorithm to the post-assessment of SINS alignment[J].Journal of Shanghai Jiaotong University, 2004, 38(10):1744-1747.

    HOU Yu-hong, LIANG Bao-hua. A Method for Obtaining Navigation Sensor Flight Testing Benchmark[J]. Electronics Optics & Control, 2014, 21(7): 95
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