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Open Access

Joint parameter and state estimation for stochastic uncertain system with multivariate skew t noises

Shuhui LIaZhihong DENGaXiaoxue FENGa( )Ruxuan HEaFeng PANa,b
School of Automation, Beijing Institute of Technology, Beijing 100081, China
Kunming-BIT Industry Technology Research Institute INC, Kunming 650106, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Due to the pulse interference, measurement outliers and artificial modeling errors, the multivariate skew t noise widely exists in the real environment. However, to date, little attention has been paid to the state estimation for systems in which the process noise and the measurement noise are both modeled as the heavy-tailed and skew non-Gaussian noise. In this paper, the multivariate skew t distribution is utilized to model the heavy-tailed and skew non-Gaussian noise. Then a probabilistic graphical form of the multivariate skew t distribution is given and proved. Based on the probabilistic graphical form, a hierarchical Gaussian state space model for stochastic uncertain systems is proposed, which transforms the estimation problem for systems with the heavy-tailed and skew non-Gaussian noises into the one with a hierarchical Gaussian state space model. Next, given the designed Gaussian state space model, the robust Bayesian filter and smoother based on the variational Bayesian inference are proposed to approximately estimate the system state and the unknown noise parameters. Furthermore, the complexity analysis together with the controllability and observability for stochastic uncertain systems with multivariate skew t noises is given. Finally, the simulation results of the target tracking scenario verify the validity of the proposed algorithms.

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Chinese Journal of Aeronautics
Pages 69-86

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Cite this article:
LI S, DENG Z, FENG X, et al. Joint parameter and state estimation for stochastic uncertain system with multivariate skew t noises. Chinese Journal of Aeronautics, 2022, 35(5): 69-86. https://doi.org/10.1016/j.cja.2021.04.032

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Received: 12 January 2021
Revised: 20 February 2021
Accepted: 20 March 2021
Published: 28 May 2021
© 2021 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).