• DocumentCode
    3572773
  • Title

    Time matching strategy for missiles attack based upon pseudo spectral optimization prediction method

  • Author

    Limin Zhang ; Mingwei Sun ; Zengqiang Chen

  • Author_Institution
    Tianjin Key Lab. of Intell. Robot., Nankai Univ., Tianjin, China
  • fYear
    2014
  • Firstpage
    1670
  • Lastpage
    1675
  • Abstract
    In the process of salvo attack of cruise missile, in order to solve the time matching problem occurring in the flight process, predicting online real-time trajectory optimization based on the pseudo spectral method under the condition of no-fly zones constraint, and the combination circular maneuver are presented. The whole route area of cruise missile is divided, and the method of forward search of no-fly zone to adjust the route online rapidly is provided. Simulation results show that the proposed method can make the cruise missile effectively consume the redundant time and bypass the no-fly zone successfully, the adjust distance is short, and can fly back to the original trajectory in the end of the adjustment, eventually achieve the goal of salvo attack.
  • Keywords
    missiles; trajectory optimisation (aerospace); combination circular maneuver; cruise missile; flight process; missiles attack; no-fly zones constraint condition; online real-time trajectory optimization prediction; pseudospectral optimization prediction method; salvo attack process; time matching strategy; Educational institutions; Intelligent control; Missiles; Optimization; Process control; Real-time systems; Trajectory; circular maneuver; no-fly zone; predicting online real-time trajectory optimization; pseudo spectral; salvo attack;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Control and Automation (WCICA), 2014 11th World Congress on
  • Type

    conf

  • DOI
    10.1109/WCICA.2014.7052971
  • Filename
    7052971