Study on Maneuvering Target Trajectory Simulation and Tracking Based on IMM algorithm

On the background of air defense missile which use radar command guidance, this article focuses on the maneuvering target trajectory simulation and tracking problem by considering possible maneuvering modes and target overload. Taking Serpentine maneuvering (S maneuvering) as an example, the target...

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Vydané v:Journal of physics. Conference series Ročník 2460; číslo 1; s. 12002 - 12009
Hlavní autori: Ma, J R, Ma, Q H, Yang, S J, Zheng, J Q, Wang, S W
Médium: Journal Article
Jazyk:English
Vydavateľské údaje: Bristol IOP Publishing 01.04.2023
Predmet:
Air defense
Algorithms
Command guidance
Kalman filters
Maneuvering targets
Missile systems
Missile tracking
Overloading
Physics
Simulation
System effectiveness
Tracking problem
ISSN:1742-6588, 1742-6596
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Shrnutí:On the background of air defense missile which use radar command guidance, this article focuses on the maneuvering target trajectory simulation and tracking problem by considering possible maneuvering modes and target overload. Taking Serpentine maneuvering (S maneuvering) as an example, the target trajectory is simulated based on overload using stepwise design method, and data are measured through sensor models. Since single model cannot model the maneuvering target motion exactly, the estimation is addressed by combining the interacting multiple model algorithm and unscented Kalman filter algorithm, so as to study the applications of maneuvering target trajectory simulation and tracking in air defense missile systems. The effectiveness of the algorithm is demonstrated with simulated data.
Bibliografia:ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 14
ISSN:1742-6588
1742-6596
DOI:10.1088/1742-6596/2460/1/012002