• DocumentCode
    1017517
  • Title

    A series representation of the spherical error probability integral

  • Author

    Del Marco, S.

  • Author_Institution
    Raytheon, Tewksbury, MA
  • Volume
    29
  • Issue
    4
  • fYear
    1993
  • fDate
    10/1/1993 12:00:00 AM
  • Firstpage
    1349
  • Lastpage
    1356
  • Abstract
    The author derives an infinite series representation of the spherical error probability integral (SEPI). The SEPI characterizes missile miss distance distributions resulting from Monte Carlo simulations. The SEPI is used when these distributions occupy a three-dimensional region of space. Truncation of this series provides a computationally efficient tool for approximating the SEPI. A series convergence analysis is presented that provides an upper bound on the approximation accuracy. The accuracy bound may be used to determine a sufficient number of terms needed for approximation to any desired accuracy. Presentation of numerical results provides empirical confirmation of the validity of the series expression. Calculation of the truncated series and numerical integration of the SEPI generate the numerical results. It is shows that the SEPI converges to the circular error probability integral as the standard deviation of a given component approaches zero. Approximation error bounds, as a function of sigma, are derived
  • Keywords
    Monte Carlo methods; convergence of numerical methods; error statistics; integration; military computing; missiles; numerical analysis; probability; series (mathematics); Monte Carlo simulations; approximation error bounds; circular error probability integral; computationally efficient tool; infinite series representation; missile miss distance distributions; numerical integration; series convergence analysis; series expression; spherical error probability integral; truncated series; Approximation error; Convergence; Error probability; Missiles; Performance analysis; System performance; Upper bound;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.259539
  • Filename
    259539