2009
DOI: 10.1109/tsp.2009.2025083
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CramÉr–Rao Bound Analysis of Positioning Approaches in GNSS Receivers

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Cited by 61 publications
(39 citation statements)
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“…In order to evaluate the estimation performance for multipath propagation, Cramer‐Rao bound, the theoretical lower bound of accuracy of any unbiased estimator, is adopted to show the potential performance of ML estimation. For a single‐path case, it is not difficult to derive that the CRB of propagation time delay τ is CRB1()τ=σ24π2A2BBf2S()fnormaldf. …”
Section: Cramer‐rao Bound For Multipath Propagationmentioning
confidence: 99%
“…In order to evaluate the estimation performance for multipath propagation, Cramer‐Rao bound, the theoretical lower bound of accuracy of any unbiased estimator, is adopted to show the potential performance of ML estimation. For a single‐path case, it is not difficult to derive that the CRB of propagation time delay τ is CRB1()τ=σ24π2A2BBf2S()fnormaldf. …”
Section: Cramer‐rao Bound For Multipath Propagationmentioning
confidence: 99%
“…It is shown that this method can mitigate multipath and jamming interferences. A Cramér-Rao Bound of position for both conventional and DPE approaches is presented in [22] in order to show DPE is better compared to the conventional one. Despite the effectiveness of the DPE technique, its implementation within a GNSS receiver remains a great difficulty since these works are still theoretical and very general.…”
Section: Collective Detectionmentioning
confidence: 99%
“…The covariance matrix of θ is constrained by the Cramer-Rao bound (CRB), which can be expressed as [11] …”
Section: Joint Navigation State Error Discriminatormentioning
confidence: 99%
“…Moreover, the element of H k in the ith row and jth column simply depends on the ith and jth elements of θ. Thus, because the x-axis, y-axis, and z-axis operate in the same way, it is reasonable to choose G 11 and H 11 as representatives for the analysis of the characteristics of the position estimation error, and to choose G 15 and H 55 to probe the characteristics of the velocity estimation error. In the case of observing four satellites, the cost function, gradient, and Hessian values for position and velocity estimation errors in the x-direction are shown in Figure 2, where all the values have been normalized.…”
Section: Iterative Maximum Likelihood Estimationmentioning
confidence: 99%