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High-dynamic GPS trackingThe results of comparing four different frequency estimation schemes in the presence of high dynamics and low carrier-to-noise ratios are given. The comparison is based on measured data from a hardware demonstration. The tested algorithms include a digital phase-locked loop, a cross-product automatic frequency tracking loop, and extended Kalman filter, and finally, a fast Fourier transformation-aided cross-product frequency tracking loop. The tracking algorithms are compared on their frequency error performance and their ability to maintain lock during severe maneuvers at various carrier-to-noise ratios. The measured results are shown to agree with simulation results carried out and reported previously.
Document ID
19890010742
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hinedi, S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Statman, J. I.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 5, 2013
Publication Date
December 15, 1988
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
NAS 1.26:184868
JPL-PUBL-88-35
NASA-CR-184868
Report Number: NAS 1.26:184868
Report Number: JPL-PUBL-88-35
Report Number: NASA-CR-184868
Accession Number
89N20113
Funding Number(s)
CONTRACT_GRANT: NAS7-918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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