Electronics Optics & Control, Volume. 27, Issue 6, 90(2020)

Design of a Controller for Hypersonic Vehicle Based on Sliding Mode Disturbance Observer

WANG Cheng and WANG Xugang
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    References(4)

    [3] [3] MCMINN J D, PINCKNEY S Z, KELLEY M L, et al.Hypersonic vehicle simulation model:winged-cone configuration, NASA-TM-102610[R].Hampton, VA, US: NASA Langley Research Center, 1990.

    [4] [4] WANG Q, STENGEL R F.Robust nonlinear control of a hypersonic aircraft[J].Journal of Guidance, Control, and Dynamics, 2000, 23(4):577-585.

    [5] [5] XU H, MIRMIRANI M D, IOANNOU P A.Adaptive sliding mode control design for a hypersonic flight vehicle[J].Journal of Guidance, Control, and Dynamics, 2004, 27(5):829-838.

    [9] [9] MARRISON C I, STENGEL R F.Design of robust control system for a hypersonic aircraft[J].Journal of Guidance, Control, and Dynamics, 1998, 21(1):58-62.

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    WANG Cheng, WANG Xugang. Design of a Controller for Hypersonic Vehicle Based on Sliding Mode Disturbance Observer[J]. Electronics Optics & Control, 2020, 27(6): 90

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    Paper Information

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    Received: Jun. 20, 2019

    Accepted: --

    Published Online: Dec. 25, 2020

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2020.06.018

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