• DocumentCode
    2047405
  • Title

    UAV Simulator-Based Simulation of Flight Control System

  • Author

    Jin Guo-dong ; Gu Liang-xian ; Lu Li-bin

  • Author_Institution
    Coll. of Astronaut., Northwestern Polytech. Univ., Xi´an
  • fYear
    2009
  • fDate
    23-24 May 2009
  • Firstpage
    1
  • Lastpage
    4
  • Abstract
    Most UAV flight control system simulation was used for evaluating the quality of UAV and designing it, however, the results failed to conform to actual flight laws. According to the need of UAV simulator in actually, a new way which was convenient for engineering computing and appropriated for simulation training was built for simulating flight control system. With the actual flight figures, flight parameters were modified by least squares method curve fitting. The system offers a way for developing UAV simulation training system, thus of great value in both theory and practice.
  • Keywords
    aerospace control; computer based training; curve fitting; least squares approximations; remotely operated vehicles; UAV simulator-based simulation; curve fitting; engineering computing; flight control system; least squares method; simulation training; unmanned aerial vehicle; Aerospace control; Aerospace engineering; Aerospace simulation; Atmosphere; Atmospheric modeling; Computational modeling; Educational institutions; Engines; Mathematical model; Unmanned aerial vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Systems and Applications, 2009. ISA 2009. International Workshop on
  • Conference_Location
    Wuhan
  • Print_ISBN
    978-1-4244-3893-8
  • Electronic_ISBN
    978-1-4244-3894-5
  • Type

    conf

  • DOI
    10.1109/IWISA.2009.5073226
  • Filename
    5073226