• DocumentCode
    736441
  • Title

    Design of multi-objective trajectory optimization with impact angle and time constraints based on fuzzy

  • Author

    Limin, Zhang ; Huizhi, Wang ; Haitao, Gao ; Weixun, Li

  • Author_Institution
    School of Mechanical Engineering, Liaoning Technical University, Fuxin, Liaoning, 123000, China
  • fYear
    2015
  • fDate
    28-30 July 2015
  • Firstpage
    3629
  • Lastpage
    3634
  • Abstract
    In order to improve the missile penetration probability, the impact angle and time of a missile should be coordinated. This paper introduces the Gauss pseudo-spectral method to the trajectory planning of a missile, and multi-objective optimal planning. Based on the mass point model of missile, the optimal trajectory planning problem, which have the constraints of terminal constraint, overload and no-fly zone constraints, is transformed to find the solution of a nonlinear programming problem by the pseudo-spectral method. The cost function was improved, according to the principle of more important target has a higher satisfaction-degree at different time, based on the optimization of the fuzzy, by adjusting the parameters to obtain the requirements of optimization and the importance rating of the optimal trajectory at the same time, realize the control of direction and time, and managed to bypass the no-fly zone, and the minimum energy consumption. Finally, missiles coordinated attack conditions are simulated. Simulation results show the effectiveness of the proposed algorithm and reference value for engineering practice.
  • Keywords
    Interpolation; Missiles; Optimal control; Trajectory optimization; Angle; fuzzy; no-fly zone; time; trajectory planning;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2015 34th Chinese
  • Conference_Location
    Hangzhou, China
  • Type

    conf

  • DOI
    10.1109/ChiCC.2015.7260200
  • Filename
    7260200