• Opto-Electronic Engineering
  • Vol. 39, Issue 9, 12 (2012)
XU Kai1、*, JIN Guang1, ZHANG Liu1, and SUN Zhi-yuan1、2
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    DOI: 10.3969/j.issn.1003-501x.2012.09.003 Cite this Article
    XU Kai, JIN Guang, ZHANG Liu, SUN Zhi-yuan. Semi-physics Simulation of Small Satellite Attitude Control in Stereo Imaging[J]. Opto-Electronic Engineering, 2012, 39(9): 12 Copy Citation Text show less
    References

    [2] Shih-Che Lo, Yon-Ping Chen. Smooth Sliding-Mode Control for Spacecraft Attitude Tracking Maneuvers [J]. Journal of Guidance, Control, and Dynamics(S0731-5090 ), 1995, 18(6): 1345-1349.

    [5] LI Chuan-jiang, MA Guang-fu, SONG Bin. Spacecraft Attitude Tracking Control Based on Nonlinear H Control [C]// Proceeding of 1st International Symposium on Systems and Control in Aerospace and Astronautics, Harbin, China, Jan 19-21, 2006: 399-403.

    [7] Wie B, Weiss H, Arapostathis A. Quaternion Feedback Regulator for Spacecraft Eigenesis Rotations [J]. Journal of Guidance, Control and Dynamics(S0731-5090), 1989, 12(3): 375-380.

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    XU Kai, JIN Guang, ZHANG Liu, SUN Zhi-yuan. Semi-physics Simulation of Small Satellite Attitude Control in Stereo Imaging[J]. Opto-Electronic Engineering, 2012, 39(9): 12
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