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Estimation of the Angular Turn Rate of an Airborne Object Based on the Unscented Transformation of an Augmented State Vector

https://doi.org/10.35596/1729-7648-2026-24-5-51-59

Abstract

A discrete filter is examined for the joint estimation of the coordinates, velocity, and angular rate W of a target performing a steady turn, based on indirect (polar/spherical) radar measurements. When W is included in the augmented state vector, the increment conversion matrix becomes a nonlinear function of W itself; consequently, linearization – as employed in previously studied versions of the extended Kalman filter for indirect measurements – requires recalculating the Jacobian matrix at each step and introduces an additional methodological error. An unscented transformation of the augmented state vector is proposed to eliminate the need for linearizing the motion and measurement models. Monte Carlo statistical simulations (Nrun = 545) were conducted to compare the proposed algorithm with its linearized counterpart across eight standard surveillance radar types (2D and 3D) and five target turn rates. The results demonstrate that the proposed algorithm yields a root-mean-square error for the W estimate that is, on average, 4.3 times lower (median 4.0; range 1.4–14.0 across all observation conditions) than that of the linearized extended Kalman filter, while offering a more modest improvement (averaging 1.2 times) in the root-mean-square error of the position estimate.

About the Authors

P. Khmarski
Institute of Applied Physics of the National Academy of Sciences of Belarus
Belarus

Khmarski Petr, Cand. Sci. (Tech.), Associate Professor, Leading Researcher  Tel.: +375 17 300-73-98

220072, Minsk, Akademicheskaya St., 16

 



V. Artemiev
Institute of Applied Physics of the National Academy of Sciences of Belarus
Belarus

Artemiev V., Corr. Member of the National Academy of Sciences of Belarus , Dr. Sci. (Tech.), Professor, Principal Researcher

Minsk



A. Naumov
Institute of Applied Physics of the National Academy of Sciences of Belarus
Belarus

Naumov A., Cand. Sci. (Phys. and Math.), Head of Laboratory

Minsk



A. Bondarenko
Military Academy of the Republic of Belarus
Belarus

Bondarenko A., Lecturer

Minsk



B. Muxammedov
Institute of Military Aviation of the University of Military Security and Defense of the Republic of Uzbekistan
Uzbekistan

Muxammedov B., Head of the Research Laboratory

Qarshi



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For citations:


Khmarski P., Artemiev V., Naumov A., Bondarenko A., Muxammedov B. Estimation of the Angular Turn Rate of an Airborne Object Based on the Unscented Transformation of an Augmented State Vector. Doklady BGUIR. 2026;24(5):51-59. (In Russ.) https://doi.org/10.35596/1729-7648-2026-24-5-51-59

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ISSN 1729-7648 (Print)
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