Chinese Space Science and Technology ›› 2015, Vol. 35 ›› Issue (4): 10-16.doi: 10.3780/j.issn.1000-758X.2015.04.002

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ResearchonPerformanceAnalysisMethodofGlobalSatelliteNavigationSystemSignal

ZHANGJianjun 1,2 XUEMing 1,2   

  1. (1ChinaAcademyofSpaceTechnology,Beijing100094)
    (2QianXuesenLaboratoryofSpaceTechnology,Beijing100094)
  • Received:2015-01-30 Revised:2015-06-01 Published:2015-08-25 Online:2015-08-25

Abstract: Sofar,computersimulationisthemainevaluationmethodforthecompatibilityperformanceofthesatellitenavigationsignals.Themodelingwasusedtosimulatethemeasuringconditionandstep,butitisimpossibletoreproducetheoperatingconditionoftherealnavigationsystem.Anyparameterchangewillleadtotheresimulation,averylargeamountofcomputationandanalysis,andlargeerrors.Basedonthesatellitenavigationreceiver,thecompatibilityofthenavigationsignalwasstudied.Firstly,themodelwasdeducedbytheratiooftheoutputsignalpowerofinstantcorrugatortothesumofthenoisepowerandtheinterferencepower,accordingtotheeffectoftheinterferencesignalonGNSSreceivercapture,carriertrackinganddataconditioning.Toobtaintheoptimalassessmentoftheinference,theequivalentcarriertonoiseratiomodelwasestablishedbyarelativelysimpleformula,basedonaspectralisolationfactor.Secondly,thepower,theantennagainandtheconstellationpowergainofthenavigationsignalswereanalyzedconcretelywhensignalarrivedatthegroundastheGPSC/Acodeself-disturbed.Finally,theattenuationtestingresultoftheequivalentcarriertonoiseratiowasshownwhentheGPSC/Acodeself-disturbed.Itprovidesreferenceforthesignaldesignofthenewsatellitenavigationsystem.

Key words: Globalsatellitenavigationsystem, Compatibility, Assessment, EquivalentCNR, Spectrumseparationcoefficient