• DocumentCode
    1940162
  • Title

    Geometry optimization for GPS navigation

  • Author

    McKay, J.B. ; Pachter, M.

  • Author_Institution
    Air Force Inst. of Technol., Wright-Patterson AFB, OH, USA
  • Volume
    5
  • fYear
    1997
  • fDate
    10-12 Dec 1997
  • Firstpage
    4695
  • Abstract
    This paper presents the analysis and numerical optimization of the geometry of an inverted pseudolite positioning system. First, the effect of geometry on the system´s accuracy is examined. The geometric dilution of precision produced by typical system geometry is considered, and an alternate measure of the geometry effect, the condition number of the “visibility” matrix H, is introduced. Next, the optimization of the system´s geometry is presented. The simplified problem of optimizing the geometry with respect to a stationary pseudolite is solved. The results of a numerical optimization are presented and both the effectiveness of the optimization routine and the usefulness of the resulting system configurations are discussed. Finally, design guidelines for good geometry are listed
  • Keywords
    Global Positioning System; aircraft navigation; attitude control; geometry; matrix algebra; optimisation; GPS navigation; aircraft; geometric sensitivity; geometry; global positioning system; inverted pseudolite positioning system; optimization; Accuracy; Aircraft navigation; Computational geometry; Equations; Global Positioning System; Guidelines; Satellite navigation systems; Testing; Transmission line matrix methods; US Government;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1997., Proceedings of the 36th IEEE Conference on
  • Conference_Location
    San Diego, CA
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-4187-2
  • Type

    conf

  • DOI
    10.1109/CDC.1997.649738
  • Filename
    649738