• Electronics Optics & Control
  • Vol. 21, Issue 7, 81 (2014)
LIU Jun, HUANG Yi-min, SUN Chun-zhen, and YIN Liang-liang
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2014.07.018 Cite this Article
    LIU Jun, HUANG Yi-min, SUN Chun-zhen, YIN Liang-liang. Roll Control and Robustness Analysis for Hypersonic Vehicle in Reentry Phase[J]. Electronics Optics & Control, 2014, 21(7): 81 Copy Citation Text show less
    References

    [1] CALHOUN P.An entry flight controls analysis for a reu-sable launch vehicle [R].AIAA-2000-1046, 2000.

    [2] MOUL M T, PAULSON J W.Dynamic lateral behavior of high-performance aircraft[R].NACA RM-L58E16, 1958.

    [3] LEE H P, CHANG M, KAISER M K.Flight dynamics and stability and control characteristics of the X-33 technology demonstrator vehicle[R].AIAA-98-4410, 1998.

    [4] WU L N, HUANG Y M, HE C L.Research on lateral control system for reusable launch vehicle in return phase[J].Journal of Nanjing University of Aeronautics & Astronautics, 2009, 41(3):329-333.

    [5] KUREEMUN R, BATES D G, HAYES M J.On the gene-ration of LFT-based uncertainty models for flight control law robustness analysis[R].AIAA-2001-4396, 2001.

    [6] TU K Y, SIDERIS A, MEASE K D, et al.Robust lateral-directional control design for the F/A-18[R].AIAA-1999-4204, 1999.

    [7] GREGORY I, MCMINN J, SHAUGHNESSY J.Hypersonic vehicle control law development using H∞ and μ-synthesis[R].AIAA-1992-5010, 1992.

    [8] LIU L.Method of assessment and confirmation for modern flight control system[M].Beijing:National Defense Industry Press, 2010.

    [9] MORTON B, MCAFOOS R.A u-test for real parameter variations[C]//Proceeding of the ACC, 1985:135-138.

    LIU Jun, HUANG Yi-min, SUN Chun-zhen, YIN Liang-liang. Roll Control and Robustness Analysis for Hypersonic Vehicle in Reentry Phase[J]. Electronics Optics & Control, 2014, 21(7): 81
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