• DocumentCode
    3364348
  • Title

    Maximum Range computation based on differential flatness for guided bombs

  • Author

    Geng, Lina ; Sun, Weimeng ; Zheng, Zhiqiang

  • Author_Institution
    Coll. of Mechatron. Eng. & Autom., Nat. Univ. of Defense Technol., Changsha, China
  • fYear
    2009
  • fDate
    9-12 Aug. 2009
  • Firstpage
    2026
  • Lastpage
    2030
  • Abstract
    The paper presents an efficient computational method for Maximum Range of guided bombs based on differential flatness. Differential flatness theory is briefly described and original motion model of guided bomb is reformulated by introducing flat outputs. The original states and inputs can be defined in terms of the flat outputs and their derivatives, and all the boundary conditions and path constraints are also mapped into the flat output space. Any curve that satisfies the boundary conditions as well as path constraints is a solution trajectory of the original system. Therefore, maximum range trajectory is planned in the flat output space. Then, the dynamic optimization problem is translated into static optimization one by collocation method. Finally, the computation approach is proved to be feasible and optimal by an initial trajectory integral that the target is set at maximum range.
  • Keywords
    missile guidance; position control; boundary conditions; collocation method; differential flatness; dynamic optimization problem; guided bombs; initial trajectory integral; maximum range computation; path constraints; static optimization; Automation; Boundary conditions; Costs; Differential equations; Mathematical model; Optimal control; Optimization methods; Performance analysis; Polynomials; Weapons; collocation method; constrained trajectory; differential flatness; guided bomb;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronics and Automation, 2009. ICMA 2009. International Conference on
  • Conference_Location
    Changchun
  • Print_ISBN
    978-1-4244-2692-8
  • Electronic_ISBN
    978-1-4244-2693-5
  • Type

    conf

  • DOI
    10.1109/ICMA.2009.5246267
  • Filename
    5246267