Parameter evaluation of complex maneuvering targets using Kalman fitering and multi-model adaptation

Authors

DOI:

https://doi.org/10.15587/1729-4061.2025.335274

Keywords:

guidance law, missile, homing, maneuvers, estimate

Abstract

The object of research is the system determines the target angular coordinates on the missile’s homing head. Current target coordinate determination systems employed in seekers often operate under significant limitations. When a target’s actual motion deviates from the simplified, hypothetical model used to synthesize the coordinate system, a critical issue arises: the errors in evaluating both the coordinates and their derivative components rapidly and significantly increase.

Problem that was solved is to evaluate complex maneuvering target parameters. But there is no need to know the target’s maneuver frequency.

This study presents a novel filtering algorithm that accurately estimates all parameters of complex maneuvering targets without prior knowledge of their maneuver frequency. The algorithm achieves a significant advantage, reducing estimation error by over 95% within the first 5 seconds. With its simple structure, high stability, and fast convergence, this robust solution is essential for modern guidance systems, greatly enhancing the effectiveness of tracking unpredictable threats.

A key strength of the proposed algorithm lies in its simple structure. Furthermore, it demonstrates high convergence rates and exceptional stability, crucial attributes for real-time applications. Its design also ensures ease of practical implementation, making it a viable solution for contemporary guidance systems.

The algorithm is built on modern control techniques, combining extended Kalman filtering with interactive multi-models. It is necessary to accurately evaluate the target’s position, velocity, acceleration, and acceleration derivative without needing to know in advance the target’s maneuver frequency

Author Biographies

Nguyen Thi Dieu Linh, Hanoi University of Industry

PhD

Department of Science and Technology

Dao Xuan Hien, Academy of Military Science and Technology

Master

Institute of Missile

Nguyen Van Bang, Air Defence – Air Force Academy

Department of Missile

References

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Parameter evaluation of complex maneuvering targets using Kalman fitering and multi-model adaptation

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Published

2025-08-30

How to Cite

Linh, N. T. D., Hien, D. X., & Bang, N. V. (2025). Parameter evaluation of complex maneuvering targets using Kalman fitering and multi-model adaptation. Eastern-European Journal of Enterprise Technologies, 4(4 (136), 83–90. https://doi.org/10.15587/1729-4061.2025.335274

Issue

Vol. 4 No. 4 (136) (2025): Mathematics and Cybernetics - applied aspects

Section

Mathematics and Cybernetics - applied aspects

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Copyright (c) 2025 Nguyen Thi Dieu Linh, Dao Xuan Hien, Nguyen Van Bang

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