• DocumentCode
    1986077
  • Title

    Design of new predictive guidance algorithm via fuzzy techniques

  • Author

    Wang, Junbo ; Ren, Zhang ; Liang, Zixuan ; Xiong, Zihao

  • Author_Institution
    Sci. & Technol. on Aircraft Control Lab., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
  • fYear
    2011
  • fDate
    16-18 Sept. 2011
  • Firstpage
    633
  • Lastpage
    637
  • Abstract
    New predictive guidance (NPG) algorithm is proposed and the fuzzy techniques are adopted to improve the real-time capability of the predictive guidance. The simplified kinematical and dynamical equations of model for the entry vehicle are established. The nominal bank angel profile is established beforehand to implement numerical prediction. The predictive errors are used as input of fuzzy logic controller which is designed for generation of correct commands. The fuzzy logic controller avoids massive iterations of conventional predictive guidance (CPG) algorithm and improves the real-time capability. Numerical simulations for the proposed algorithm under the condition of perturbations are presented to demonstrate the capability and effectiveness.
  • Keywords
    fuzzy control; missile guidance; predictor-corrector methods; dynamical equations; fuzzy logic controller; fuzzy techniques; kinematical equations; new predictive guidance algorithm; numerical simulations; Algorithm design and analysis; Atmospheric modeling; Prediction algorithms; Real time systems; Trajectory; Vehicle dynamics; Vehicles; Entry vehicles; entry guidance; fuzzy logic controller; predictive guidance;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electrical and Control Engineering (ICECE), 2011 International Conference on
  • Conference_Location
    Yichang
  • Print_ISBN
    978-1-4244-8162-0
  • Type

    conf

  • DOI
    10.1109/ICECENG.2011.6057648
  • Filename
    6057648