Electronics Optics & Control, Volume. 20, Issue 1, 49(2013)

Attitude and Momentum Control of Agile Satellite Using DGCMG

CUI Peiling1...2,3 and ZHANG Ying1,23 |Show fewer author(s)
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  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    References(5)

    [1] [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] [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] [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] [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] [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.

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    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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    Paper Information

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    Received: Aug. 24, 2012

    Accepted: --

    Published Online: Jan. 24, 2013

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2013.01.012

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