• DocumentCode
    2258298
  • Title

    An improved nonlinear guidance law for unmanned aerial vehicles path following

  • Author

    Hui, Mao Yun ; Yang, Chen Qing ; Xi, Hou Zhong ; Zheng, Guo

  • Author_Institution
    Institute of Nearspace Technology, College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, China, 410073
  • fYear
    2015
  • fDate
    28-30 July 2015
  • Firstpage
    5271
  • Lastpage
    5276
  • Abstract
    To guarantee the UAVs path following accuracy and guarantee the ability of anti-disturbance, an improved nonlinear path following method for UAVs is proposed in the paper. Based on the nonlinear guidance logic, the virtual target on the path is confirmed and the instantaneous lateral acceleration of UAVs is calculated. What´s more, to compensate other uncertain factors in the path following process such as model uncertainty or other disturbances (wind etc), a feed-back term is added accordingly. Simulations are carried out, including the straight line and curved circle path following experiments, to verify the advantages of the proposed method.
  • Keywords
    Acceleration; Aerospace control; Aerospace engineering; Electronic mail; Trajectory; Vehicle dynamics; Vehicles; Feedback term; Nonlinear guidance logic; Path following;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2015 34th Chinese
  • Conference_Location
    Hangzhou, China
  • Type

    conf

  • DOI
    10.1109/ChiCC.2015.7260462
  • Filename
    7260462