• DocumentCode
    2898162
  • Title

    DME/P critical area determination on message passing processors [microwave landing system mathematical model]

  • Author

    Celenk, M. ; Dibenedetto, M. ; Rajendran, J.

  • Author_Institution
    Ohio Univ., Athens, OH, USA
  • fYear
    1992
  • fDate
    23-27 Mar 1992
  • Firstpage
    261
  • Lastpage
    268
  • Abstract
    The authors discuss research whose objective is to optimize the simulation process required for development of the precision distance measuring equipment (DME/P) critical area guidance material. This material is developed from the analysis of error contour plots, which provide the guidance system errors along the desired approach path due to signal scattering from a surface vehicle. The contour data are generated by executing the microwave landing system (MLS) mathematical model considering an interfering surface vehicle positioned at selected locations on an M×N grid and analyzing the model data as described. Optimal grid spacing is necessary to accurately describe the errors as a function of surface vehicle location while minimizing the simulation time required. A method based on the two-dimensional fast Fourier transform is described to estimate the spatial frequency spectrum of the contour data. Once spectral estimates become available, the optimal grid spacing is obtained using the Nyquist sampling theorem. To further reduce the overall processing time of this task, parallel processing is desired. A technique for parallel implementation on a Symult S-2010 message passing system is presented
  • Keywords
    aerospace computing; computerised navigation; distance measurement; fast Fourier transforms; message passing; microwave landing systems; microwave measurement; optimisation; radiofrequency interference; radionavigation; DME/P critical area determination; MLS; Nyquist sampling theorem; Symult S-2010 message passing system; contour data; error contour plots; guidance system errors; mathematical model; message passing processors; microwave landing system; optimal grid spacing determination; parallel implementation; precision distance measuring equipment; signal scattering; simulation; spatial frequency spectrum; surface vehicle; two-dimensional fast Fourier transform; Area measurement; Error analysis; Frequency estimation; Mathematical model; Mesh generation; Message passing; Navigation; Scattering; Signal analysis; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Position Location and Navigation Symposium, 1992. Record. 500 Years After Columbus - Navigation Challenges of Tomorrow. IEEE PLANS '92., IEEE
  • Conference_Location
    Monterey, CA
  • Print_ISBN
    0-7803-0468-3
  • Type

    conf

  • DOI
    10.1109/PLANS.1992.185853
  • Filename
    185853