• Electronics Optics & Control
  • Vol. 21, Issue 7, 19 (2014)
LI Wei-xing, LI Xiu-juan, LI Chun-tao, and YANG Yi
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2014.07.005 Cite this Article
    LI Wei-xing, LI Xiu-juan, LI Chun-tao, YANG Yi. A Robust Adaptive Control Law Design Method for Flying-Wing UAV[J]. Electronics Optics & Control, 2014, 21(7): 19 Copy Citation Text show less
    References

    [1] WISE K A.Bank-to-turn missile autopilot design using loop transfer recovery[J].Journal of Guidance, Control, and Dynamics, 1990, 13(1):145-152.

    [2] CAO C Y, HOVAKIMYAN N.Guaranteed transient performance with L1 adaptive controller for systems with unknown time-varying parameters and bounded disturbances[C]//American Control Conference, 2007, ACC07, IEEE, 2007:3925-3930.

    [3] CAO C Y, HOVAKIMYAN N.L1 adaptive output feedback controller for systems with time-varying unknown parameters and bounded disturbances[C]//Proceedings of the American Control Conference, 2007:486-491.

    [4] WISE K A, EUGENE L, ZIMMERMAN J, et al.Adaptive flight control of a sensor guided munition[C]//AIAA Guidance, Navigation, and Control Conference, San Francisco, USA, 2005, AIAA-2005-6385.

    [5] WISE K A.EUGENE L, HOVAKIMYAN N.Adaptive control of flight:Theory, applications, and open problems[C]//American Control Conference, IEEE 2006:doi:10.1109/ACC.2006.1657677.

    LI Wei-xing, LI Xiu-juan, LI Chun-tao, YANG Yi. A Robust Adaptive Control Law Design Method for Flying-Wing UAV[J]. Electronics Optics & Control, 2014, 21(7): 19
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