Abstract

The Kalman filter requires knowledge of the noise statistics; however, the noise covariances are generally unknown. Although this problem has a long history, reliable algorithms for their estimation are scant, and necessary and sufficient conditions for identifiability of the covariances are in dispute. We address both of these issues in this paper. We first present the necessary and sufficient condition for unknown noise covariance estimation; these conditions are related to the rank of a matrix involving the auto and cross-covariances of a weighted sum of innovations, where the weights are the coefficients of the minimal polynomial of the closed-loop system transition matrix of a stable, but not necessarily optimal, Kalman filter. We present an optimization criterion and a novel six-step approach based on a successive approximation, coupled with a gradient algorithm with adaptive step sizes, to estimate the steady-state Kalman filter gain, the unknown noise covariance matrices, as well as the state prediction (and updated) error covariance matrix. Our approach enforces the structural assumptions on unknown noise covariances and ensures symmetry and positive definiteness of the estimated covariance matrices. We provide several approaches to estimate the unknown measurement noise covariance R via post-fit residuals, an approach not yet exploited in the literature. The validation of the proposed method on five different test cases from the literature demonstrates that the proposed method significantly outperforms previous state-of-the-art methods. It also offers a number of novel machine learning motivated approaches, such as sequential (one sample at a time) and mini-batch-based methods, to speed up the computations.

Highlights

  • INTRODUCTIONThe Kalman filter (KF) [23] is the optimal state estimator for linear dynamic systems driven by Gaussian white noise

  • The Kalman filter (KF) [23] is the optimal state estimator for linear dynamic systems driven by Gaussian white noiseThe associate editor coordinating the review of this manuscript and approving it for publication was Pietro Savazzi .with measurements corrupted by Gaussian white noise.1 In the classical design of a Kalman filter, the noise covariance matrices are assumed known and they, along with the system dynamics, determine the achievable filter’s accuracy

  • Following the ideas in [49], we prove that the necessary and sufficient condition to estimate the unknown covariance matrices in a system is directly related to its minimal polynomial of

Read more

Summary

INTRODUCTION

The Kalman filter (KF) [23] is the optimal state estimator for linear dynamic systems driven by Gaussian white noise. 2) A novel six-step solution approach via a successive approximation and adaptive gradient descent scheme with a new objective function to obtain the unknown noise covariance matrices Q and R, as well as the steady-state Kalman filter gain W , and the steady-state state prediction covariance matrix Por the updated state covariance matrix P, is proposed. This ensures positive definite Q and positive definite R, as well as Pand P. The iteration variable is superscript with (·) to differentiate the notation from exponents

PLANT AND MEASUREMENT MODEL FOR THE KALMAN FILTER
APPROACHES TO OBTAIN FILTER PARAMETERS
ESTIMATION OF W
STEP 6
SPECIAL CASES
CASE 1
NUMERICAL EXAMPLES
CASE 3
Findings
CASE 4 with
Full Text
Paper version not known

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call