2021
DOI: 10.1080/00207179.2020.1870158
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Adaptive Kalman filtering for closed-loop systems based on the observation vector covariance

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Cited by 9 publications
(6 citation statements)
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“…The conditions of the theorem, with the exception of the last one, are well known and provide the existence of the steadystate of the KF. The fulfillment of condition (d) and the restriction on the choice of 𝜇 guarantees the monotonic behavior of the solutions of the matrix equations under consideration (18), (21).…”
Section: Monotonicity Properties Of the Rhofir Filtermentioning
confidence: 99%
See 1 more Smart Citation
“…The conditions of the theorem, with the exception of the last one, are well known and provide the existence of the steadystate of the KF. The fulfillment of condition (d) and the restriction on the choice of 𝜇 guarantees the monotonic behavior of the solutions of the matrix equations under consideration (18), (21).…”
Section: Monotonicity Properties Of the Rhofir Filtermentioning
confidence: 99%
“…In general, the Bayesian approach is computationally intractable due to the numerical integration over a large parameter space. In maximum likelihood estimation [19][20][21][22][23][24], the noise statistics are obtained by maximizing the probability density function of the measurement residuals generated by the filter, which is the likelihood of the noise parameters. Adaptive filters based on maximum likelihood methods require nonlinear optimization and are computationally intractable.…”
Section: Introductionmentioning
confidence: 99%
“…However, the satellite clock and receiver clock cannot be fully synchronized within the BeiDou standard time, resulting in time errors. Not only need to solve specific spatial location, to solve the receiver clock is poor, so in the observation point must be at least four visible satellites to according to the equations to solve the specific position [5]. This article only choose four satellites, pseudorange positioning formula is as follows: In the formula, 𝑹 represents the pseudo range from satellite to receiver; (𝑿, 𝒀, 𝒁) represents the satellite spatial position coordinates; (𝒙 𝒖 , 𝒚 𝒖 , 𝒛 𝒖 ) indicates the estimated position of the point to be measured; 𝒄 is the speed of light; 𝜹𝒕 𝒖 is the receiver clock error.…”
Section: Beidou System Pseudorange Positioning Principlementioning
confidence: 99%
“…The adaptive filter, while filtering measured data, concurrently estimates some system model parameters, utilizing limited, indirect, and noisy measurements to infer information that is challenging to measure or ascertain directly [ 30 ]. The adaptive filtering method further encompasses the output error method, innovation method, Sage–Husa method [ 31 ], strong tracking filtering method, and adaptive robust and second-order [ 32 ] mutual difference method [ 31 ], among others. These methods have been effectively employed in the engineering field.…”
Section: Introductionmentioning
confidence: 99%