• Electronics Optics & Control
  • Vol. 20, Issue 11, 31 (2013)
ZHANG Chuantao, LIU Chunsheng, and HAN Hongwen
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2013.11.007 Cite this Article
    ZHANG Chuantao, LIU Chunsheng, HAN Hongwen. A Novel Adaptive Sliding Mode Control Framework Applied to Morphing Aircraft[J]. Electronics Optics & Control, 2013, 20(11): 31 Copy Citation Text show less
    References

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    [3] LIU ChunshengLI ChuntaoHE Zhe.Adaptive control of a morphing aircraft through updating the number of actuators[C]// AIAA GuidanceNavigationand Control Conference1316 August 2012MinneapolisMinnesota.AIAA 2012-4446.

    [4] POPOV A VGRIGORIE T LBOTEZ R Met al.Modeling and testing of a morphing wing in openloop architecture[J].Journal of Aircraft201047(3):917-923.

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    [12] RUBAGOTTI MESTRADA ACASTANOS Fet al.Integral sliding mode control for nonlinear systems with matched and unmatched perturbations [J].IEEE Transactions on Automatic Control201156(11):2699-2704.

    ZHANG Chuantao, LIU Chunsheng, HAN Hongwen. A Novel Adaptive Sliding Mode Control Framework Applied to Morphing Aircraft[J]. Electronics Optics & Control, 2013, 20(11): 31
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