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A comparison of frequency estimation techniques for high-dynamic trajectoriesA comparison is presented for four different estimation techniques applied to the problem of continuously estimating the parameters of a sinusoidal Global Positioning System (GPS) signal, observed in the presence of additive noise, under extremely high-dynamic conditions. Frequency estimates are emphasized, although phase and/or frequency rate are also estimated by some of the algorithms. These parameters are related to the velocity, position, and acceleration of the maneuvering transmitter. Estimated performance at low carrier-to-noise ratios and high dynamics is investigated for the purpose of determining the useful operating range of an approximate Maximum Likelihood (ML) estimator, an Extended Kalman Filter (EKF), a Cross-Product Automatic Frequency Control (CPAFC) loop, and a digital phase-locked loop (PPL). Numerical simulations are used to evaluate performance while tracking a common trajectory exhibiting high dynamics.
Document ID
19890011016
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Vilnrotter, V. A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hinedi, S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Kumar, R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 5, 2013
Publication Date
September 15, 1988
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
JPL-PUBL-88-21
NASA-CR-184865
NAS 1.26:184865
Report Number: JPL-PUBL-88-21
Report Number: NASA-CR-184865
Report Number: NAS 1.26:184865
Accession Number
89N20387
Funding Number(s)
CONTRACT_GRANT: NAS7-918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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