• DocumentCode
    1795112
  • Title

    Unmanned helicopter control based on trim predication technology

  • Author

    Zhirong Lei ; Long Shi ; Jia Li ; Dongliang Song

  • Author_Institution
    Sch. of Autom., Northwestern Polytech. Univ., Xian, China
  • fYear
    2014
  • fDate
    8-10 Aug. 2014
  • Firstpage
    1368
  • Lastpage
    1372
  • Abstract
    This paper discusses the application of trim prediction technology which is used to design unmanned helicopter control laws. Trim prediction technology takes “implicit integrator” replace integrator appears explicitly in the PID control laws. For the first time, this paper adopts and applys the trim prediction technology to design unmanned helicopter control laws. According to simulation results, compared with traditional PID control laws, the simulation results are similar with PID control, but trim prediction technology can overcome disadvantages of traditional PID. The effectiveness of trim prediction control laws is documented through simulation. and shows that trim prediction technology can be used on unmanned helicopter.
  • Keywords
    aircraft control; autonomous aerial vehicles; control system synthesis; helicopters; position control; three-term control; PID control law; implicit integrator; trim predication technology; unmanned helicopter control; Attitude control; Computers; Helicopters; PD control; Real-time systems; Software;
  • 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.2014.7007396
  • Filename
    7007396