2020
DOI: 10.1109/access.2020.3031978
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A Framework of Cubature-Hᵢ/H-Fault Detection and Robust H-Infinity Kalman Filter of Ship SINS/GNSS Integrated System

Abstract: This paper deals with the problem of considering both robust fault detection and accurate state estimation for a strapdown inertial navigation system and global navigation satellite system (SINS/GNSS)integrated navigation system for ships within a unified framework. Under the assumption that the process disturbance and measurement noise being 2 l-norm bounded, a cubature / i HH  fault detection filter (FDF) considering both sensitivity and robustness to disturbance is proposed to detect faults with a postfilt… Show more

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Cited by 7 publications
(6 citation statements)
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“…The initial state covariance . In this case, the overall performance x E of CKF [11], HCKF [35], GCLCKF and AGCLCKF for various states of generator are shown in TABLE Ⅰ. It can be easily noted that the x E of GCLCKF and AGCLCKF is much smaller than that of CKF and HCKF.…”
Section: A Case 1: Gaussian Noise Distribution Conditionsmentioning
confidence: 93%
See 1 more Smart Citation
“…The initial state covariance . In this case, the overall performance x E of CKF [11], HCKF [35], GCLCKF and AGCLCKF for various states of generator are shown in TABLE Ⅰ. It can be easily noted that the x E of GCLCKF and AGCLCKF is much smaller than that of CKF and HCKF.…”
Section: A Case 1: Gaussian Noise Distribution Conditionsmentioning
confidence: 93%
“…where MC N , S N and T N represent the total number of Monte Carlo runs, state variables and simulation time, respectively; In order to verify and highlight the efficacy of the proposed method, the methods CKF [11], HCKF [35], and the developed GCLCKF are utilized to make comparisons under the different circumstances.…”
Section: Illustrative Examplementioning
confidence: 99%
“…Step 3: Two coefficient matrices are calculated using (20) and ( 21), and the cubature point error is calculated using (18). Finally, the new error is obtained using (23). The difference between the CKF and the ICKF is shown in figure 1 in red.…”
Section: Calculate Process For Ickfmentioning
confidence: 99%
“…Different adaptive methods were used to improve the performance of the filter. These adaptive factors can be generated by a method based on either the sensor measurement noise variance or complex mathematical methods, such as the H-infinity strategy [23], M-estimation theory [24], and maximum likelihood [25]. Unfortunately, these methods either suffer from a low rank in the matrix or involve human experience, which makes them difficult to apply in practical scenarios.…”
Section: Introductionmentioning
confidence: 99%
“…An approximately optimal H∞ filter was found by constantly adjusting the parameter γ during target tracking [11]. A method to adjust γ to its minimum at each iteration in the framework of unscented transformation was presented in [12,18], and a similar strategy was used in [19][20][21] to generate adaptive H∞ Kalman filters. An optimal robust H∞ estimator was obtained by minimising the H∞ norm from uncertain disturbances to estimation errors by using the convex optimisation method [22].…”
Section: Introductionmentioning
confidence: 99%