Electronics Optics & Control, Volume. 27, Issue 1, 85(2020)

Attitude Control of Fixed-Wing UAV Under Model Uncertainty and Disturbances

TANG Yu1... LIN Da2,3, CAO Lijia1 and LIU Yongchun2 |Show fewer author(s)
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
  • show less

    Firstly, the attitude dynamic model of the fixed-wing UAV under ideal conditions is given, and then, the UAV attitude controller is designed based on the dynamic inverse method.But the controller above is not suitable for the UAV model under actual conditions, because there is a certain offset between the actual model and the ideal model, which is model uncertainty.Moreover, there are also some external disturbances in the actual situation.Therefore, the fuzzy neural network is combined with the original UAV attitude controller to compensate for the model uncertainty and external disturbances existed in the operation of the UAV.

    Tools

    Get Citation

    Copy Citation Text

    TANG Yu, LIN Da, CAO Lijia, LIU Yongchun. Attitude Control of Fixed-Wing UAV Under Model Uncertainty and Disturbances[J]. Electronics Optics & Control, 2020, 27(1): 85

    Download Citation

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

    Category:

    Received: Mar. 7, 2019

    Accepted: --

    Published Online: Dec. 23, 2020

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2020.01.017

    Topics