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Publishing Language: Chinese

Target trajectory tracking and extrapolation based on INT-VSMM algorithm

Xuanming REN1Xinmin TANG2( )Yusheng LIU1Qixing LU1
College of Civil Aviation,Nanjing University of Aeronautics and AstronauticsNanjing 211106China
School of Transportation Science and Engineering,Civil Aviation University of ChinaTianjin 300300China
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Abstract

In order to address the issue of the traditional variable structure multiple model (VSMM) algorithm's lengthy computation time and difficulty meeting real-time constraints, we developed the intent variable structure multiple model (INT-VSMM) algorithm. This algorithm uses the target state and flight intent data collected by automatic dependent surveillance-broadcast (ADS-B) as the model’s priori data, combining it with the VSMM theoretical framework. The motion pattern of the target in the flight phase of the flight path is decomposed, and a complete set of motion models is established. According to the principle of directed graph switching, a model set switching method is designed, which is mainly based on "hard" switching and supplemented by "soft" switching. The INT-VSMM algorithm is used to track the trajectory of the target aircraft, and short-term trajectory extrapolation is performed based on the target state estimation. According to the simulation results, the INT-VSMM algorithm outperforms the compared current approaches in terms of target tracking performance and computing time. Additionally, the extrapolated trajectory has a lower short-term inaccuracy, which can satisfy conflict detection requirements.

CLC number: V249 Document code: A Article ID: 1001-5965(2026)01-0203-11

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Journal of Beijing University of Aeronautics and Astronautics
Pages 203-213

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Cite this article:
REN X, TANG X, LIU Y, et al. Target trajectory tracking and extrapolation based on INT-VSMM algorithm. Journal of Beijing University of Aeronautics and Astronautics, 2026, 52(1): 203-213. https://doi.org/10.13700/j.bh.1001-5965.2023.0724

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Received: 05 November 2023
Published: 27 December 2023
© Journal of Beijing University of Aeronautics and Astronautics