• DocumentCode
    3112133
  • Title

    A linearized model for the line of sight guidance law

  • Author

    Belkhouche, E. ; Belkhouche, B. ; Rastgoufard, P.

  • Author_Institution
    Electr. Eng. & Comput. Sci. Dept., Tulane Univ., New Orleans, LA, USA
  • fYear
    2004
  • fDate
    26-29 April 2004
  • Firstpage
    201
  • Lastpage
    207
  • Abstract
    This paper deals with the linearization of the nonlinear model describing the kinematics equations of the line of sight guidance law. The linearized model is derived based on optimization techniques, where different cost functions are used. It turns out that in the case of maneuvering targets, the linear coefficients are time independent and time dependent in the case of maneuvering targets. In both cases these coefficients depend on the initial line of sight angle, which means that the linearization has the same order as the nonlinear system. The linearization method is illustrated using simulation, and a comparison with the classical linearization is provided.
  • Keywords
    missile guidance; navigation; cost functions; kinematics equations; line of sight guidance law; linear coefficients; linearized model; nonlinear model; optimization techniques; Aerodynamics; Cost function; Game theory; Kinematics; Modems; Motion control; Nonlinear equations; Nonlinear systems; Optimal control; Process control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Position Location and Navigation Symposium, 2004. PLANS 2004
  • Print_ISBN
    0-7803-8416-4
  • Type

    conf

  • DOI
    10.1109/PLANS.2004.1308994
  • Filename
    1308994