• DocumentCode
    2908020
  • Title

    Upper bound on C/A and L1C code spectral separation coefficients

  • Author

    Raghavan, Srini H. ; Powell, Thomas D.

  • Author_Institution
    Aerosp. Corp., Los Angeles, CA, USA
  • fYear
    2011
  • fDate
    5-12 March 2011
  • Firstpage
    1
  • Lastpage
    5
  • Abstract
    It is well known that the available effective carrier-to-noise density ratio (C/N0)effective to a GPS receiver is degraded to a greater degree due to spectral line effects than when spectral line effects are ignored for the Global Positioning System (GPS) coarse acquisition (C/A) codes. 12(C/N0)effective is an important parameter used to characterize the GPS receiver performance in terms of code acquisition, carrier loss of lock, and data bit error rate. In today´s signal environment, which includes a growing number of Global Navigation Satellite Systems (GNSSs) in the Radio Navigation Satellite System (RNSS) band, there is a need to account for all the interference sources accurately to make sure that the intersystem and intrasystem Radio Frequency Compatibility (RFC) is achieved. Towards this goal many studies in the past considered quasi-analysis and simulation methods to account for the spectral line effects on the GPS C/A code receivers. The spectral separation coefficient (SSC) provides a measure of the amount of interference that can be expected from one signal to the other. An upper bound on C/A code SSC was presented in last year´s IEEE Aeroconference [1]. In this paper we make refinements to the upper bound equations for the C/A codes presented in [1] and also extend the bounds to codes other than the C/A codes. Computational advantage is still retained with the refinement to the equations.
  • Keywords
    Global Positioning System; codes; C/A code; GNSS; GPS receiver; IEEE Aeroconference; L1C code spectral separation coefficients; RFC; RNSS; SSC; carrier-to-noise density ratio; coarse acquisition codes; global navigation satellite systems; global positioning system; radio frequency compatibility; radio navigation satellite system; Equations; Global Positioning System; Interference; Noise; Receivers; Satellites; Upper bound;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2011 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-7350-2
  • Type

    conf

  • DOI
    10.1109/AERO.2011.5747363
  • Filename
    5747363