• Electronics Optics & Control
  • Vol. 20, Issue 1, 49 (2013)
CUI Peiling1、2、3 and ZHANG Ying1、2、3
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2013.01.012 Cite this Article
    CUI Peiling, ZHANG Ying. Attitude and Momentum Control of Agile Satellite Using DGCMG[J]. Electronics Optics & Control, 2013, 20(1): 49 Copy Citation Text show less
    References

    [1] VADALI S R WALKER S R OH H S.Preferred gimbal angles for single gimbal control moment gyros[J].Journal of Guidance Control and Dynamics 1990 13:1090-1095.

    [2] FANG J C REN Y.High-precision control for a single-gimbal magnetically suspended control moment gyro based on inverse system method[J].IEEE Transaction on Industrial Electronics 2011 58(9):4331-4342.

    [3] WIE B.Singularity analysis and visualization of single-gimbal control moment gyros system[J].Journal of Guidance Control and Dynamics 2004 27(2):271-282.

    [5] VADALI S R OH H S.Space station attitude control and moment management:A nonlinear look[J].Journal of Guidance Control and Dynamic 1992 15(3):568-577.

    [7] WIE B BAILEY D HEIBERG C.Singularity robust steering logic for redundant single-gimbal gontrol moment gyros[J].Journal of Guidance Control and Dynamic 2001 24(5):865-872.

    CUI Peiling, ZHANG Ying. Attitude and Momentum Control of Agile Satellite Using DGCMG[J]. Electronics Optics & Control, 2013, 20(1): 49
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