• DocumentCode
    1794828
  • Title

    Automatic landing on carrier method of unmanned air vehicle

  • Author

    Lu Ke ; Wang Zhengzhong ; Yuan Suozhong

  • Author_Institution
    Sci. & Technol. on Rotorcraft Aeromechanics Lab., Jingdezhen, China
  • fYear
    2014
  • fDate
    8-10 Aug. 2014
  • Firstpage
    299
  • Lastpage
    302
  • Abstract
    Automated carrier landing of an Unmanned Air Vehicle is a complex process. To successfully complete the task of landing on carrier, firstly the guidance system should give UAV flight control system a proper landing trajectory, then the flight control system according to the instructions given by the guidance system of UAV make the UAV fly on the right track, finally realizing automatic landing on carrier. In this process the guidance system providing correct guidance signal is a key factor in the success of landing on carrier. Now most aircraft carriers have angled deck, so there are great differences to ground-based landing. In view of this situation, a guidance law is designed for UAV landing on carrier, and the simulation of guidance law is carried out. Because of the air flow disturbance behind of the carrier, the requirement of flight control system is robust, so, this paper introduces quantitative feedback robust control design method to design the flight controller, in order to guarantee the robustness of control system. The results show that the guidance law and flight control system designed in this paper could realize the UAV autonomous landing.
  • Keywords
    aerospace simulation; aircraft landing guidance; autonomous aerial vehicles; control system synthesis; feedback; robust control; trajectory control; UAV flight control system; UAV landing; air flow disturbance; aircraft carriers; angled deck; automated carrier landing; carrier method; flight controller design; ground-based landing; guidance law simulation; guidance signal; guidance system; landing trajectory; quantitative feedback robust control design method; robustness; unmanned air vehicle; Aerospace control; Aircraft; Control systems; Design methodology; Educational institutions; Global Positioning System; Robustness;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
  • Conference_Location
    Yantai
  • Print_ISBN
    978-1-4799-4700-3
  • Type

    conf

  • DOI
    10.1109/CGNCC.2014.7007248
  • Filename
    7007248