Electronics Optics & Control, Volume. 23, Issue 6, 50(2016)

An Attitude Control Method of Kinetic Kill Vehicle Based on Eigenaxis Rotation

LIU Wei, CHEN Yuan-bao, and WANG Xuan
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    References(6)

    [3] [3] WEN J T, KREUTZ-DELGADO K. The attitude control problem[J]. IEEE Transactions on Automatic Control, 1991, 36(10): 1148-1162.

    [5] [5] LAM Q, PAL P, HU A, et al. Robust attitude control using a joint quaternion feedback regulator and nonlinear model-follower[C]//AIAA/AAS Astrodynamics Conference, San Diego, 1996: 817-827.

    [6] [6] LIZARRALDE F, WEN J T. Attitude control without angular velocity measurement a passivity approach[J]. IEEE Transactions on Automatic Control, 1996, 41(3): 468-472.

    [7] [7] WIE B, BARBA P M. Quaternion feedback for spacecraft large angle maneuvers[J]. Journal of Guidance, Control, and Dynamics, 1985, 8(3): 360-365.

    [8] [8] TAYEBI A. Unit quaternion-based output feedback for the attitude tracking problem[J]. IEEE Transactions on Automatic Control, 2008, 53(6): 1516-1520.

    [9] [9] WIE B, WEISS H, ARAPOSTATHIS A. Quarternion feedback regulator for spacecraft eigenaxis rotations[J]. Journal of Guidance, Control, and Dynamics, 1989, 12(3): 375-380.

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    LIU Wei, CHEN Yuan-bao, WANG Xuan. An Attitude Control Method of Kinetic Kill Vehicle Based on Eigenaxis Rotation[J]. Electronics Optics & Control, 2016, 23(6): 50

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    Paper Information

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    Received: Apr. 29, 2015

    Accepted: --

    Published Online: Jan. 28, 2021

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2016.06.011

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