2018
DOI: 10.1134/s2075108718040089
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Sigma-Point Kalman Filter Algorithm in the Problem of GNSS Signal Parameters Estimation in Non-Coherent Tracking Mode in Spacecraft Autonomous Navigation Equipment

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Cited by 5 publications
(2 citation statements)
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“…In this case, other approaches have been considered that use several different strategies for approaching the optimal solution. These approaches are suboptimal and include the extended Kalman filter (EKF) and unscented Kalman filter (UKF) [11][12][13][14][15][16][17][18][19]. In this variant, a suboptimal nonlinear tracking filter (EKF or UKF) replaces both the discriminator and the tracking loop filter.…”
Section: Introductionmentioning
confidence: 99%
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“…In this case, other approaches have been considered that use several different strategies for approaching the optimal solution. These approaches are suboptimal and include the extended Kalman filter (EKF) and unscented Kalman filter (UKF) [11][12][13][14][15][16][17][18][19]. In this variant, a suboptimal nonlinear tracking filter (EKF or UKF) replaces both the discriminator and the tracking loop filter.…”
Section: Introductionmentioning
confidence: 99%
“…This algorithm gives a more correct solution to nonlinear problems as compared with the EKF and forms suboptimal estimates of the state vector according to the criterion of the minimum meansquare error of the estimate. The authors of [16,17] proposed an SPKF algorithm in the problem of GPS signal parameter estimation in coherent and noncoherent tracking modes in spacecraft autonomous navigation equipment. The obtained results suggested that the SPKF algorithm could form RNP estimates with appropriate accuracy under the conditions of space consumer functioning.…”
Section: Introductionmentioning
confidence: 99%