• DocumentCode
    233027
  • Title

    The application of proportional navigation in the process of UAV air combat guidance and optimization of proportional parameter

  • Author

    Wang Hui ; Guan Zuoyu ; Yu Lijun

  • Author_Institution
    Coll. of Autom., Harbin Eng. Univ., Harbin, China
  • fYear
    2014
  • fDate
    28-30 July 2014
  • Firstpage
    7892
  • Lastpage
    7896
  • Abstract
    The authors propose a concept of effective attack range to follow the active attacking of Unmanned Aerial Vehicle. An improved proportional navigation model is suggested for being used in the air combat Unmanned Aerial Vehicle guidance model. In addition, the value of proportional parameter is calculated in nonlinear guidance model, and the optimal proportional parameter is confirmed. The simulation results show that the proposed model is effective and quickly.
  • Keywords
    aircraft landing guidance; aircraft navigation; autonomous aerial vehicles; optimisation; proportional control; air combat UAV guidance model; nonlinear guidance model; optimal proportional parameter optimisation; proportional navigation model; unmanned aerial vehicle; Decision support systems; Trajectory; Attack range; Unmanned Aerial Vehicle; optimal parameter; proportional guidance law;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2014 33rd Chinese
  • Conference_Location
    Nanjing
  • Type

    conf

  • DOI
    10.1109/ChiCC.2014.6896318
  • Filename
    6896318