2014
DOI: 10.12732/ijpam.v91i1.4
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Convergence Analysis of Extended Kalman Filter in a Noisy Environment Through Difference Equations

Abstract: In this paper, the convergence aspects of the Extended Kalman Filter, when used as a deterministic observer for a nonlinear discrete-time systems, are addressed and analyzed. The conditions needed to ensure the boundedness of the error covariances which are related to the observability properties of the nonlinear systems are identified through difference equations. Furthermore, boundedness and stability conditions are provided in a noisy environment systems.

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Cited by 10 publications
(9 citation statements)
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“…In this estimation process, the system state matrix is always A n = I 2 and the system observation matrix is always C n = 1 . Hence, according to theory (3.4) in Elizabeth and Ramakrishnan (2015), the KF is a global asymptotic observer as long as the noise matrix W = ( left left b ^ left 0 left1 0 left c ^ ) has rank (2), which is always true, and ( R , Q ) are positive definite matrices.…”
Section: Qov Semi-active Suspension Problem Formulationmentioning
confidence: 99%
See 1 more Smart Citation
“…In this estimation process, the system state matrix is always A n = I 2 and the system observation matrix is always C n = 1 . Hence, according to theory (3.4) in Elizabeth and Ramakrishnan (2015), the KF is a global asymptotic observer as long as the noise matrix W = ( left left b ^ left 0 left1 0 left c ^ ) has rank (2), which is always true, and ( R , Q ) are positive definite matrices.…”
Section: Qov Semi-active Suspension Problem Formulationmentioning
confidence: 99%
“…Here, | | A | | = sup { A n , n = 0 , 1 , 2 , . . } and | | C | | = sup { C n , n = 0 , 1 , 2 , . . } are bounded due to states bound limits, Q , R are positive definite, and noise matrix W = W 1 W 1 T (see Equation (12)) is of rank (5), hence the KF observer is asymptotic according to theory (3.4) in Elizabeth and Ramakrishnan (2015).…”
Section: Qov Active Suspension Problem Formulationmentioning
confidence: 99%
“…where n is the total number of GPS devices, idealValue is the IDEAL weight value from CnW-S1, h fused is the fused EC and GPS heading value, h allGPS is the fused calculated heading for all the "n" number of GPS, w allGPS is the weight given to calculated combined GPS heading, h EC is the measured EC heading, w EC is the weight given to EC heading, w i is the weight given to "i th " GPS, h i is the calculated FAz heading of "i th " GPS, and * h fused is labeled as "GPSEC_yaw" in the later parts of algorithm and it will also be used in lieu of GPSn_FAz during the EKF stage when GPS data is invalid. The controllability and observability of the extended Kalman filter or Kalman filter have been extensively researched and proven in several works such as those by Elizabeth and Jothilakshmi [45], Kamrani et al [46], and Southall et al [47]. The dynamic and measurement models which are nonlinear in nature are as follows:…”
Section: Classification and Weighing-stage 1 (Cnw-s1mentioning
confidence: 99%
“…In [25] better convergence was obtained by using the normal form of the governing ordinary differential equations. Local asymptotic convergence of the estimation error with an assumption of observability of the nonlinear system was subsequently shown in [20], [21].…”
Section: Introductionmentioning
confidence: 98%
“…Local asymptotic convergence of the estimation error under an observability assumption of the nonlinear system has been shown in [20], [21]. In [22], conditions for asymptotic convergence are imposed on the linearization residues.…”
Section: Introductionmentioning
confidence: 99%