• Electronics Optics & Control
  • Vol. 21, Issue 12, 67 (2014)
LIU Yi-ning1, GUO Jian-guo1, ZHOU Jun1, and WANG Guo-qing2
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2014.12.015 Cite this Article
    LIU Yi-ning, GUO Jian-guo, ZHOU Jun, WANG Guo-qing. Design of Integral Type Terminal Sliding Mode Controlling Method for Hypersonic Vehicle Based on Disturbance Observer[J]. Electronics Optics & Control, 2014, 21(12): 67 Copy Citation Text show less
    References

    [1] LANE S H,STENGEL R F.Flight control design using non-linear inverse dynamics[J].Automatica,1988,24(4): 471-483.

    [2] VAN OORT E R,SONNEVELDT L,CHU Q P,et al.Full-envelope modular adaptive control of a flighter aircraft using orthogonal least aquares[J]. Journal of Guidance, Control,and Dynamics,2010,33(5):1461-1472.

    [3] SHARMA M,RICHARDS N D.Adaptive integrated gui-dance and control for missile interceptors[R].AIAA-2004-4880,2004.

    [4] PU M,WU Q X,JIANG C S,et al.New fast terminal sli-ding mode and its application to near space vehicles[J].Acta Aeronautica et Astronautica Sinica,2011,32(7):1283-1291.

    [5] ZONG Q,WANG J,TIAN B L,et al.Quasi-continuous high-order sliding mode controller and observer design for flexible hypersonic vehicle[J].Aerospace Science and Technology,2013,27:127-137.

    [6] ZHANG T Y,ZHOU J,GUO J G.Disign of predictive controller for hypersonic vehicles based on disturbance observer[J].Acta Aeronautica et Astronautica Sinica,2014, 35(1):215-222.

    [7] KESHMINI S,COLGREN R,MIRMIRANI M.Six DOF nonlinear equations of motion for a generic hypersonic vehicle[R]. AIAA-2007-6626,Reston:AIAA,2007.

    LIU Yi-ning, GUO Jian-guo, ZHOU Jun, WANG Guo-qing. Design of Integral Type Terminal Sliding Mode Controlling Method for Hypersonic Vehicle Based on Disturbance Observer[J]. Electronics Optics & Control, 2014, 21(12): 67
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