• DocumentCode
    835551
  • Title

    Accurate solution of proportional navigation for maneuvering targets

  • Author

    Mahapatra, R. ; Shukla, U.S.

  • Author_Institution
    Dept. of Aerosp. Eng., Indian Inst. of Sci., Bangalore, India
  • Volume
    25
  • Issue
    1
  • fYear
    1989
  • Firstpage
    81
  • Lastpage
    89
  • Abstract
    An accurate solution is presented of the nonlinear differential equations describing motion under proportional navigation when the target is laterally maneuvering. A quasilinearization (QL) approach is used, followed by a perturbation technique to obtain closed-form solutions for trajectory parameters. An explicit expression for the pursuer lateral acceleration is derived and shown to contain contributions due to initial heading error and target maneuver, with a coupling between the two effects. The solution is shown to be a substantial and consistent generalization or an earlier accurate solution for nonmaneuvering targets and also of classical linear solutions for maneuvering targets. The generalized QL solution presented provides very accurate estimates of pursuer lateral acceleration over a much broader range of engagement geometries and target maneuvers than presently available closed-form solutions.<>
  • Keywords
    military systems; nonlinear differential equations; proportional control; closed-form solutions; laterally maneuvering targets; missile guidance; nonlinear differential equations; perturbation technique; proportional navigation; quasilinearization; trajectory parameters; Acceleration; Closed-form solution; Force control; Geometry; Linear approximation; Motion analysis; Motion control; Navigation; Nonlinear equations; Perturbation methods;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.18664
  • Filename
    18664