Electronics Optics & Control, Volume. 20, Issue 11, 31(2013)

A Novel Adaptive Sliding Mode Control Framework Applied to Morphing Aircraft

ZHANG Chuantao... LIU Chunsheng and HAN Hongwen |Show fewer author(s)
Author Affiliations
  • [in Chinese]
  • show less

    A novel adaptive integral sliding mode tracking controller is proposed for a morphing aircraft.The adaptive compensation algorithm is used to dispel the effect of parametric uncertainty on system stability.The perturbation can be projected into the matched and unmatched spaces.The additional integral term in the sliding surface reduces the steady state error and also provides one more degree of freedomwhich minimizes the Hinfinity norm of unmatched perturbation.It is shown that the stability of the closedloop system can be guaranteed with the proposed adaptive sliding mode control strategy.The feasibility of designed control scheme is demonstrated by a morphing aircraft model application.

    Tools

    Get Citation

    Copy Citation Text

    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

    Download Citation

    EndNote(RIS)BibTexPlain Text
    Save article for my favorites
    Paper Information

    Category:

    Received: Nov. 21, 2012

    Accepted: --

    Published Online: Dec. 4, 2013

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2013.11.007

    Topics