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EKF-based target estimation for the APN missile guidance using a YOLO-driven seeker
ID Hodžić, Mirza (Author), ID Prljača, Naser (Author)

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Abstract
Sodobni zakoni vodenja takticnih raket zahtevajo natan ˇ cno ˇ sledenje cilju in ocenjevanje njegovega stanja za ucinkovito ˇ prestrezanje manevrirajocih ciljev. Proporcionalna navigacija ˇ je eden najpogosteje uporabljenih zakonov vodenja, ki temelji na meritvah hitrosti spremembe smerne crte za generiranje ˇ bocnih pospeškov. Rakete obi ˇ cajno uporabljajo elektroopti ˇ cne ˇ ali infrardece iskalnike. V naši raziskavi uporabljamo dvoosni ˇ kardaniziran kamerni iskalnik z laserskim merilnikom razdalje, opremljen z algoritmom YOLO za zaznavanje, sledenje in prepoznavanje ciljev v realnem casu. Iskalnik omogo ˇ caˇ zajem slike, zaznavanje cilja, sledenje ter merjenje hitrosti spremembe smerne crte glede na inercialni koordinatni sis- ˇ tem. Poleg tega uporabljamo razširjeni Kalmanov filter za filtriranje meritev in oceno tridimenzionalnega gibanja cilja ter bocnih pospeškov. Te ocene nato uporabimo pri razširjeni ˇ proporcionalni navigaciji, ki v primerjavi s standardno zmanjša potrebne bocne pospeške rakete. Rezultati raziskave so potrjeni ˇ z nelinearnim modelom rakete s šestimi stopnjami prostosti in kažejo ucinkovitost povezovanja sledenja cilju na osnovi ˇ globokega ucenja s sodobnimi zakoni vodenja.

Language:Slovenian
Work type:Article
Typology:1.01 - Original Scientific Article
Organization:FE - Faculty of Electrical Engineering
Year:2026
Number of pages:Str. 44-55
Numbering:Letn. 93, št. 1-2
PID:20.500.12556/RUL-183221 This link opens in a new window
UDC:623.465.2:681.518.5
ISSN on article:0013-5852
COBISS.SI-ID:280851203 This link opens in a new window
Publication date in RUL:08.06.2026
Views:158
Downloads:101
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Record is a part of a journal

Title:Elektrotehniški vestnik
Publisher:Strokovna zadruga koncesijoniranih elektrotehnikov, Elektrotehniška zveza Slovenije
ISSN:0013-5852
COBISS.SI-ID:742916 This link opens in a new window

Licences

License:CC BY 4.0, Creative Commons Attribution 4.0 International
Link:http://creativecommons.org/licenses/by/4.0/
Description:This is the standard Creative Commons license that gives others maximum freedom to do what they want with the work as long as they credit the author.

Secondary language

Language:English
Title:Ocenjevanje cilja z razširjenim Kalmanovim filtrom za vodenje rakete APN z uporabo iskalnika YOLO
Abstract:
Modern tactical missile guidance laws require an accurate target tracking and state estimation to effectively intercept maneuvering targets. The Proportional Navigation (PN) is one of the most widely used guidance laws for tactical missiles, relying on line-of-sight (LOS) rate measurements to generate lateral acceleration commands. Missiles typically employ electro-optical or infrared seekers. Our study utilizes a two-axis gimbaled camera seeker which employs a laser range finder, equipped with the YOLO algorithm for a real-time target detection tracking and recognition. The seeker provides the image acquisition, target detection, tracking, and LOS rate measurement relative to the inertial frame. Additionally, an Extended Kalman Filter (EKF) is used to filter the LOS rate measurements and to estimate the target three-dimensional motion, as well as lateral accelerations. The estimates are then used to implement the Augmented Proportional Navigation (APN) which reduces the required missile lateral acceleration compared to the standard PN guidance. The study findings are validated using a six-degrees-of-freedom (6-DOF) nonlinear missile model, demonstrating its effectiveness when integrating the deep-learning-based target tracking with the modern guidance laws.

Keywords:EKF, missile guidance, YOLO, 6DOF, APN, seeker

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