• Electronics Optics & Control
  • Vol. 21, Issue 6, 56 (2014)
XU Cheng1, LUO Hang2, and HAN Bing2
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • show less
    DOI: 10.3969/j.issn.1671-637x.2014.06.012 Cite this Article
    XU Cheng, LUO Hang, HAN Bing. Zero-Effort Miss Based Terminal Guidance Law Design Using Sliding Mode Approach[J]. Electronics Optics & Control, 2014, 21(6): 56 Copy Citation Text show less
    References

    [1] YE L M.Climb-dive attack style based on proportional guidance law with angular constraint[J].Ship Science and Technology, 2011, 33(11):42-46.

    [2] CHANG C, LIN D F, QI Z K, et al.Study on the optimal terminal guidance law with interception and impact angle [J].Ship Science and Technology, 2009, 29(3):233-236, 239.

    [3] JEON I S, LEE J I, TANK M J.Impact time control gui-dance law for anti ship missiles[J].Control Systems Technology, 2006, 14(2):260-266.

    [4] WANG X H, ZHANG M L.Researching and accompli-shing for homing missile attacking maneuvering target[J].Acta Aeronautica Et Astronautica Sinica, 2000, 21(1):30-33.

    [5] BRIERLEY S D, LONGCHAMP R.Application of sliding-mode control to air-air interception problem[J].Aerospace and electronic systems, 1990, 26(2):306-325.

    [6] LIN C L, CHEN Y Y.Design of fuzzy logic guidance law against high speed target[J].Journal of Guidance, Control, and Dynamics, 2000, 23(1):17-25.

    [7] LIU Y S, LIU Z Z, LI L C.Research on fuzzy variable structure guidance law for passive homing missiles against maneuvering targets[J].Systems Engineering and Electronics, 2007, 29(2):254-258.

    [8] ZHOU R, ZHANG P.Robust guidance law design for homing missiles using neural networks[J].Acta Aeronautica Et Astronautica, 2002, 23(3):262-264.

    [9] LIU J K.The sliding structure control of Matlab simulation[M].2nd ed.Beijing: Tsinghua University Press, 2012: 1-2, 26-39.

    [10] WU P.Guidance method research with terminal attack angle constraints[D].Harbin: Harbin Institute of Technology, 2009.

    [11] HARL N, BALAKRISHNAN S N.Impact time and angle guidance with sliding mode control[J].Control systems technology, 2012, 20(6):1436-1448.

    XU Cheng, LUO Hang, HAN Bing. Zero-Effort Miss Based Terminal Guidance Law Design Using Sliding Mode Approach[J]. Electronics Optics & Control, 2014, 21(6): 56
    Download Citation