• Electronics Optics & Control
  • Vol. 27, Issue 8, 69 (2020)
PENG Zheng, NIE Hong, LI Chuntao, and ZHANG Ming
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2020.08.014 Cite this Article
    PENG Zheng, NIE Hong, LI Chuntao, ZHANG Ming. Design of Longitudinal Carrier Landing Control Law for UAVs Under Air Wake Disturbance[J]. Electronics Optics & Control, 2020, 27(8): 69 Copy Citation Text show less

    Abstract

    To solve the problem that the ship′s wake causes large carrier landing error of UAVs,dynamic inversion and the adaptive control method are used to design an automatic carrier landing control law.The control law can overcome the uncertainty of the model and external disturbances,achieve good tracking results of pitch rate and angle of attack,and guarantee the boundedness of the adaptive parameters through the projection operator.The trajectory tracking controller based on dynamic inversion is used to achieve accurate trajectory control and reduce the tracking error of ship landing.The simulation results show that the proposed control method has high tracking accuracy and good robustness,and can meet the longitudinal control requirements of UAV′s carrier landing under air wake.
    PENG Zheng, NIE Hong, LI Chuntao, ZHANG Ming. Design of Longitudinal Carrier Landing Control Law for UAVs Under Air Wake Disturbance[J]. Electronics Optics & Control, 2020, 27(8): 69
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