• DocumentCode
    2441575
  • Title

    An exact conversion from an Earth-centered coordinate system to latitude, longitude and altitude

  • Author

    Sudano, John J.

  • Author_Institution
    Lockheed Martin Gov. Electron. Syst., Moorestown, NJ, USA
  • Volume
    2
  • fYear
    1997
  • fDate
    14-18 Jul 1997
  • Firstpage
    646
  • Abstract
    Present combat systems are being upgraded to properly meet the new capabilities being developed against tactical ballistic missiles. The local coordinate systems are being upgraded to a global (WGS-84) coordinate system so that the correct exchange of threat information with other defending units can be done correctly and in a timely manner. This coordinate system upgrade is also used to properly track these threats, The computation of an Earth-centered coordinate (XECC, YECC, ZECC) system for a track referenced by altitude, latitude, and longitude is straightforward in biaxial (WGS-84) ellipsoid Earth. The problem arises using the Earth-centered coordinate system for the inverse operation to recompute the altitude, latitude and longitude of the track. This computation can only be done approximately. This article introduces a unique analytic derivation to calculate exactly the latitude, longitude, and altitude of a track from an Earth centered coordinate system. The problem is transformed into solving for a root of an eighth-order polynomial, which can then be reduced and solved by rewriting as a quartic equation. A robust, iterative numerical algorithm for computer implementation is also presented for platforms having computational and memory constraint. An example is given and comparisons made to show the application of these techniques
  • Keywords
    Newton-Raphson method; military computing; missiles; Earth-centered coordinate; Earth-centered coordinate system; altitude; biaxial (WGS-84) ellipsoid Earth; combat systems; computational constraint; computer implementation; eighth-order polynomial; global coordinate system; inverse operation; iterative numerical algorithm; latitude; longitude; memory constraint; quartic equation; tactical ballistic missile; tactical ballistic missiles; threat information; Earth; Ellipsoids; Equations; Government; Iterative algorithms; Military computing; Missiles; Polynomials; Robustness; Sea measurements;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace and Electronics Conference, 1997. NAECON 1997., Proceedings of the IEEE 1997 National
  • Conference_Location
    Dayton, OH
  • Print_ISBN
    0-7803-3725-5
  • Type

    conf

  • DOI
    10.1109/NAECON.1997.622711
  • Filename
    622711