2020
DOI: 10.1109/taes.2019.2920045
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Dual-Satellite Geolocation With Ephemeris Correction and Uncertainty Mapping

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Cited by 8 publications
(2 citation statements)
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“…We next find the approximate posterior of the state vector x k and biases in b, q(x k , b), using the obtained posterior of the precision matrices Λ i , q(Λ i ), given in (20). Again, evaluating the integral in (14) and discarding the terms that are not dependent on x k or b, simplify the ELBO into 21) where γ i,k is equal to, after applying (16),…”
Section: Outlier-robust Skfsmentioning
confidence: 99%
See 1 more Smart Citation
“…We next find the approximate posterior of the state vector x k and biases in b, q(x k , b), using the obtained posterior of the precision matrices Λ i , q(Λ i ), given in (20). Again, evaluating the integral in (14) and discarding the terms that are not dependent on x k or b, simplify the ELBO into 21) where γ i,k is equal to, after applying (16),…”
Section: Outlier-robust Skfsmentioning
confidence: 99%
“…The SKF has attracted a significant amount of attention due to its wide applications in e.g., orbit determination [12], Mars entry navigation [13] and source geolocation when satellite ephemeris errors are present [14]. In [15], it was established theoretically that the SKF is an unbiased state estimator under linear Gaussian state-space models.…”
Section: Introductionmentioning
confidence: 99%