• DocumentCode
    982416
  • Title

    Closed-form solution of pure proportional navigation

  • Author

    Becker, Klaus

  • Author_Institution
    Forschungsinst. fuer Funk & Math., Wachtberg-Werthhoven, West Germany
  • Volume
    26
  • Issue
    3
  • fYear
    1990
  • fDate
    5/1/1990 12:00:00 AM
  • Firstpage
    526
  • Lastpage
    533
  • Abstract
    The closed-form solution of the equations of motion of an ideal missile pursuing a nonmaneuvering target according to the pure proportional navigation law is obtained as a function of the polar coordinates for all real navigation constants N⩾2. The solution is given in the form of a uniformly convergent infinite product which reduces to a product of a finite number of factors if the navigation constant is a rational number. The solution is discussed, and necessary and sufficient conditions are stated for vanishing, bounded, and unbounded missile acceleration in the final phase of pursuit
  • Keywords
    missiles; navigation; acceleration; closed-form solution; differential equations; equations of motion; missiles guidance; nonmaneuvering target; polar coordinates; pure proportional navigation; pursuit; trajectories; Acceleration; Closed-form solution; Differential equations; Equations; Erbium; Geometry; Missiles; Navigation; Nonlinear systems; Sufficient conditions; Virtual manufacturing;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.106131
  • Filename
    106131