Chinese Space Science and Technology ›› 2012, Vol. 32 ›› Issue (5): 34-39.doi: 10.3780/j.issn.1000-758X.2012.05.006
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JIN Tian, WANG Li-Hua, HUANG Bing-Sheng
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Abstract: FrequencydriftcausedbyoscillatorwillpollutecarrierphaseandDopplerfrequencyinGPSreceiver.Therefore,itisnecessarytomodeltheoscillatorerrorinthetrackingsystem.TheflickernoiseerrorofoscillatorcannotbeexactlymodeledinKalmansystem,whichcauseserrorsinthemodeloftraditionalKalmanbasedtrackingloop.Tosolvetheseproblems,thefrequencydomainmodelandnoisecovarianceofoscillatorwereanalyzed,andamethodofexactlymodellingtheflickernoiseintheKalmanbasedtrackingloopwasproposed.RealGPSsatellitedatawasprocessedbyusingthenewoscillatormodeltoverifythevalidity.
Key words: Trackingloop, Crystaloscillatornoise, Kalmanfiltering, Errormodeling, Globalpositioningsystem
JIN Tian, WANG Li-Hua, HUANG Bing-Sheng. ModelingMethodforOscillatorFlickerNoiseinKalmanbasedGPSTrackingLoop[J]. Chinese Space Science and Technology, 2012, 32(5): 34-39.
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URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2012.05.006
https://journal26.magtechjournal.com/kjkxjs/EN/Y2012/V32/I5/34