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Absolute displacement estimation error 

Absolute displacement estimation error 

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Square-root cubature Kalman filter (SCKF) is more effective for nonlinear state estimation than an unscented Kalman filter. In this paper, we study the design of nonlinear filters based on SCKF for the system with one step noise correlation and abrupt state change. First, we give the SCKF that deals with the one step correlation between process and...

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... simulation results are given in Fig. 3, Fig. 4, and Table 2. The results show that SCKF-STF can achieve a better tracking effect besides the target state with abrupt change, and the tracking performance of SCKF is reduced because the abrupt state change will harm its estimation accuracy. ...

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Citations

... The adaptive current statistical (CS) model and the improved interacting multiple model (IMM) were combined with the SRCKF respectively in [11], [12], which effectively improved the maneuvering target tracking accuracy. The second is to develop adaptive filtering algorithms to obtain better filter precision, among which the strong tracking filter (STF) based on the fading memory filtering theory [13]- [16] can effectively resist the bad influence of model errors. On the other hand, it is necessary to use robust techniques for controlling the measurement outliers such as the Huber-based Kalman filter (HKF) [17] and the robust UKF with gain correction [18], [19]. ...
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... This type of STF-based method has drawn attention from many researchers. [23][24][25][26][27][28][29][30][31][32] Based on the theoretical relationship between state prediction covariance matrix and crosscovariance matrix, Wang et al. 23 obtained the equivalent calculation method of Jacobian matrix in UKF, and then established the equivalent calculation method of fading factor in nonlinear filtering algorithms. Equivalent calculation avoids the dependence of strong tracking UKF on the Jacobian matrix, and expands its applicable scale. ...
... For this reason, the fading factor is introduced into the state prediction covariance, which can force Eq. (5) to hold. The recursive equations of TSTCKF can be represented as follows: 28 (1) Suppose that the state estimationx k and the state covariance matrix P k at the moment k of the system are known. (2) Time updating Calculate the state predictionx kþ1jk and the state prediction covariance P s kþ1jk at the moment k þ 1 usingx k and P k : ...
... These two introduction methods are both used in the current researches, 23,24,31 and there are not clear differences between the two methods. 28 Therefore, Q kþ1 is ignored from the analysis. Then, the value of c kþ1 and k 2 1;kþ1 will decide whether the two fading factor calculation methods are equivalent or not. ...
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... However, the performance of the nonlinear filters will be greatly influenced when faced with the inaccurate model or bad measurement caused by the aircraft maneuver. In order to improve the tracking stability on the abrupt change, references [19]- [25] introduce the fading factor in the state error covariance matrix and structure the strong tracking (ST) nonlinear filter. However, the fading factor in [19]- [25] has two problems. ...
... In order to improve the tracking stability on the abrupt change, references [19]- [25] introduce the fading factor in the state error covariance matrix and structure the strong tracking (ST) nonlinear filter. However, the fading factor in [19]- [25] has two problems. The first is the arbitrariness of the introduced position, which is due to a lack of mathematical deduction to the simultaneous satisfaction of the orthogonality principle of residual error sequences and of the least mean-square error of the output estimation. ...
... Last but not the least, two simulation scenarios conducted show that the proposed algorithm is able to accurately track highly maneuvering motion and weak maneuvering motion at the condition of lacking prior knowledge. The performance of the proposed algorithm is better than the multiple-fading-factor SCKF [24] based on the CS model and the SCKF-STF [25] based on the modified CS model [6]. Moreover, the proposed algorithm decreases the runtime by 40% while maintaining the commensurate performance compared with the interacting-multiple-model SCKF (IMM-SCKF). ...
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... For the first case, literatures [21,22] have, respectively, proposed the networked STF and STF with randomly delayed measurements (STF/RDM). For the second case, a novel nonlinear filter derived from square-root CKF and the idea of STF was proposed in [23]. However, when the above two cases exist simultaneously, these existing STFs [17][18][19][20][21][22][23] are not suitable for dealing with the filtering problem in the above two coupled cases, and little attention has been paid to the study of deriving the corresponding STF. ...
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... (1) and (2) and the modified DUKF described by Eqs. (4)-(8), (10)- (13), and (25). Let the following assumptions hold for every k ≥ 0. ...
... The bearings-only tracking system [25] is also considered to verify the effectiveness of the proposed technique. The bearings-only tracking system is composed of two sensors to track a moving target, where each sensor obtains only an angle measurement related to the system state. ...
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... However, the cumbersome calculation of Jacobian matrices and linearization errors would degrade its performance. Some versions of nonlinear STF utilizing sigma points have been derived, but some linearization steps still exist in the given procedures (Ge et al. 2011; Yang et al. 2011 ). In this subsection , the formation of fading factor will be embedded in STF into the framework of SUKF without linearization. ...
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... As is known to all, Bearings-only tracking is a representatively passive tracking problem and it is very popular in current research on target tracking all the time (Li and Ge, 2010;Musicki et al.,2012;Ge and Li, 2011). Actually, the nature of Bearings-only tracking is nonlinear filtering and fusion. ...
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... For decades, many research findings have been obtained in the field of maneuvering target localization and tracking (Blom and Bar-Shalom, 1988;Li and Bar-Shalom, 1993;Munir and Atherton, 1995;Li et al., 2006;Peng, 2007;Zhang and Chen, 2010;Messaoudi et al., 2010;Foo and Ng, 2011;Ge et al., 2011;Zhang et al., 2012). Current research is focused mainly on the multiple model method, which is generally thought to be the best method for maneuvering target tracking (Magill, 1965;Blom and Bar-Shalom, 1988;Li and Bar-Shalom, 1993;Munir and Atherton, 1995;Xu et al., 2003;Zhu, 2008;Liu et al., 2009;Foo and Ng, 2011;Yuan and Zheng, 2011). ...
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The trajectory of a shipborne radar target has a certain complexity, randomness, and diversity. Tracking a strong maneuvering target timely, accurately, and effectively is a key technology for a shipborne radar tracking system. Combining a variable structure interacting multiple model with an adaptive grid algorithm, we present a variable structure adaptive grid interacting multiple model maneuvering target tracking method. Tracking experiments are performed using the proposed method for five maneuvering targets, including a uniform motion — uniform acceleration motion target, a uniform acceleration motion — uniform motion target, a serpentine locomotion target, and two variable acceleration motion targets. Experimental results show that the target position, velocity, and acceleration tracking errors for the five typical target trajectories are small. The method has high tracking precision, good stability, and flexible adaptability.
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