2020
DOI: 10.1063/5.0019305
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The robust residual-based adaptive estimation Kalman filter method for strap-down inertial and geomagnetic tightly integrated navigation system

Abstract: When noise statistical characteristics of the system are unknown and there are outliers in the measurement information, the filtering accuracy of the strap-down inertial navigation system/geomagnetic navigation system (SINS/GNS) tightly integrated navigation system would decrease, and the filtering may diverge in severe cases. To solve this problem, a robust residual-based adaptive estimation Kalman filter (RRAEKF) method is proposed. In the RRAEKF method, the covariance matching technique is employed to detec… Show more

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Cited by 8 publications
(10 citation statements)
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“…In the complicated platform such as manipulating unmanned aerial vehicles, state estimation is a challenge due to inherent couplings, nonlinearities, and uncertainties, so that the extended Kalman filter might not be applicable. The other form of this filter that includes two options of the unscented Kalman filter, is employed to address the state estimation problem [16]. The improvement in estimation accuracy, overall control performance, and algorithm execution time compared to the other extended Kalman filters is solidly confirmed.…”
Section: Problem Statementmentioning
confidence: 97%
“…In the complicated platform such as manipulating unmanned aerial vehicles, state estimation is a challenge due to inherent couplings, nonlinearities, and uncertainties, so that the extended Kalman filter might not be applicable. The other form of this filter that includes two options of the unscented Kalman filter, is employed to address the state estimation problem [16]. The improvement in estimation accuracy, overall control performance, and algorithm execution time compared to the other extended Kalman filters is solidly confirmed.…”
Section: Problem Statementmentioning
confidence: 97%
“…) −1 s lj k+1 (20) ξ k+1 follows the Chi-square distribution with degree of freedom m if the assumption holds. The significance level is set as γ, which indicates the probability threshold that the null hypothesis below this threshold will be rejected.…”
Section: Measurement Anomaly Detectionmentioning
confidence: 99%
“…Since the innovation vectorz i (k i ) obeys zero-mean Gaussian distribution, we can obtain from (24) that…”
Section: Fault Detectionmentioning
confidence: 99%
“…In [23], a new adaptive Kalman filter has studied for multi-sensor integrated navigation system. Recently, a new technique has been designed in [24] to handle unknown noise statistical characteristics of system and outliers in the measurement information.…”
Section: Introductionmentioning
confidence: 99%