2018
DOI: 10.1109/access.2018.2808170
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Adaptive Strong Tracking Square-Root Cubature Kalman Filter for Maneuvering Aircraft Tracking

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Cited by 53 publications
(36 citation statements)
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“…The smoothing performance index is derived using (35). We assume that x o,k contains noise with variance B x and the target moves with a constant jerk because the α-β-γ-δ filter uses the constant-jerk motion model, as indicated in (4). Thus, the true motion assumed in (35) is…”
Section: Derivation Of Smoothing Performance Indexmentioning
confidence: 99%
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“…The smoothing performance index is derived using (35). We assume that x o,k contains noise with variance B x and the target moves with a constant jerk because the α-β-γ-δ filter uses the constant-jerk motion model, as indicated in (4). Thus, the true motion assumed in (35) is…”
Section: Derivation Of Smoothing Performance Indexmentioning
confidence: 99%
“…Here, to calculate the steady-state bias error (mean error), we assume that the mean error in x o,k becomes zero because of the white Gaussian noise. Thus, X o (z) = Z[s c (kT) 4 /24] is satisfied. By substituting (A13) and (A11) into (A14), we obtain…”
Section: Conflicts Of Interestmentioning
confidence: 99%
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