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    Journals >Electronics Optics & Control >Volume 23 >Issue 3 >Page 87 > Article
    • Electronics Optics & Control
    • Vol. 23, Issue 3, 87 (2016)
    A Satellite Attitude Determination Algorithm Based on Four-Mode Differential Laser Gyro and Star Sensor
    ZANG Qiang1, GAO Jing-min1, YANG Hong-bo1, GUAN Xin2, and CHEN Shou-lei2
    Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2016.03.020 Cite this Article
    ZANG Qiang, GAO Jing-min, YANG Hong-bo, GUAN Xin, CHEN Shou-lei. A Satellite Attitude Determination Algorithm Based on Four-Mode Differential Laser Gyro and Star Sensor[J]. Electronics Optics & Control, 2016, 23(3): 87 Copy Citation Text show less
    References

    [3] TAKANORI I.High-bandwidth attitude determination using jitter measurements and optimal filtering［C］//AIAA Gui-dance, Navigation, and Control Conference, Chicago:American Institute of Aeronautics and Astronautics, 2009:14-21.

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    ZANG Qiang, GAO Jing-min, YANG Hong-bo, GUAN Xin, CHEN Shou-lei. A Satellite Attitude Determination Algorithm Based on Four-Mode Differential Laser Gyro and Star Sensor[J]. Electronics Optics & Control, 2016, 23(3): 87
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