• Title/Summary/Keyword: Active Electronically Scanned Array

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A Study on Radiator of VHF-Band Active Electronically Scanned Array with the Trapezoidal Dipole Structure Using Meander-Line (미엔더 라인을 이용한 사다리꼴 다이폴 구조의 VHF 대역 능동 위상 배열안테나 복사소자 연구)

  • Park, Dae-Sung;Ko, Young-Kwan;Choi, Jae-Hoon
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.27 no.12
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    • pp.1027-1035
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    • 2016
  • In this paper, the method to miniaturize the radiating element of a VHF-band active electronically scanned array is proposed. The length of the proposed dipole having trapezoidal shape structure is miniaturized using meander line while the performance degradation is minimized. The grid reflector is used to improve the antenna directivity and insensitivity due to the outer environment. In addition, the antenna is designed to take into account for array application. The fabricated antenna has a 9.1 % fractional bandwidth for the voltage standing wave ratio(VSWR) 2:1 and the maximum gain of 4.24 dBi. The front-to-back ratio(FBR) is larger than 15 dB.

Multiple Target Management of Air-to-Air mode on Airborne AESA Radar (항공기 탑재 AESA 레이다의 공대공 모드 다표적 관리 기법)

  • Yong-min Kim;Ji-eun Roh
    • Journal of Advanced Navigation Technology
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    • v.27 no.5
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    • pp.580-586
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    • 2023
  • AESA radar is able to instantaneously and adaptively position and control the beam, and this enables to greatly improve multi-target tracking capability with high accuracy in comparison to traditional mechanically-scanned radar system. This paper is primarily concerned with the development of an efficient methodology for multi-target managenent with the context of multi-target environment employing AESA radar. In this paper, targets are stratified into two principal categories: currently displayed targets and non-display targets, predicated upon their relative priority. Displayed targets are subsequently stratified into TOI (target of interest), HPT (high priority target), and SAT (situational awareness target), based on the requisite levels of tracking accuracy. It also suggests rules for determining target priority management, especially in air-to-air mode including interleaved mode. This proposed approach was tested and validated in a SIL (system integration lab) environment, applying it to AESA radars mounted on aircraft.

Study on 2×2 Subarray Antenna for Implementation of VHF Band Active Electronically Scanned Array (VHF 대역 능동 위상 배열안테나 구현을 위한 2×2 부배열 안테나 설계에 관한 연구)

  • Kim, Sungpeel;Han, Junyong;Jang, Younhui;Choi, Jaehoon
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.29 no.6
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    • pp.473-476
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    • 2018
  • Herein, a $2{\times}2$ subarray antenna is designed to implement a VHF band active electronically scanned array. The Yagi-Uda antenna is used as a radiating element. The bandwidth enhancement and miniaturization of the Yagi-Uda antenna are achieved by optimizing the diameter of a driven element and the length of a director. In addition, the grid reflector is utilized to improve the front-to-back ratio(FBR) and to reduce both the wind resistance and overall system weight. The fabricated $2{\times}2$ subarray antenna fully covers the VHF target band($0.98{\sim}1.02f_c$). The measured maximum gain is 10.61 dBi and the FBR is larger than 26 dB.

Design and Implementation of Radar Resource Management Algorithms for Airborne AESA Radar (항공기 탑재 능동 위상배열 레이더의 자원관리 알고리즘 설계 및 구현)

  • Roh, Ji-Eun;Chon, Sang-Mi;Ahn, Chang-Soo;Jang, Seong-Hoon
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.24 no.12
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    • pp.1190-1197
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    • 2013
  • AESA(Active Electronically Scanned Array radar) radar is able to instantaneously and adaptively position and control the beam, and such adaptive beam pointing of AESA radar enables to remarkably improve the multi-mission capability. For this reason, radar resource management(RRM) becomes new challenging issue. RRM is a technique efficiently allocating finite resources, such as energy and time to each task in an optimal and intelligent way. This paper deals with a design of radar resource management algorithms and simulator implemented main algorithms for development of airborne AESA radar. In addition, evaluation results show that developed radar system satisfies a main requirement about simultaneous multiple target tracking and detection by adopting proposed algorithms.

Domestic Environment Analysis for Building FTB Aircraft with AESA Radar (AESA Radar 탑재 FTB 항공기 구축을 위한 국내환경 분석)

  • Park, Jehong;Hong, Gyoyoung;Eom, Jeonghwan;Chong, Pilhan;Hong, Seungbeom
    • Journal of Advanced Navigation Technology
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    • v.24 no.1
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    • pp.9-15
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    • 2020
  • Recently, active electronically scanned array (AESA) radar, electro-optical and infrared (EO-IR) and infra-red search and track (IRST) sensors are under development in the Korean fighter experimental(KF-X) project, and AESA radar is currently undergoing preliminary research for flight testing. This paper focuses on the flying test bed (FTB) aircraft operation cases of developed countries in accordance with AESA radar development. As a result, we review domestic laws and regulations related to the airworthiness for FTB aircraft to operate in domestic environment and look for ways to operate FTB aircraft. Therefore, we propose how to selecting, airworthiness and operating FTB aircraft suitable for the domestic environment.

Modeling and Simulation of Aircraft Motion for Performance Assessment of Airborne AESA Radar Considering Wind and Vibration (바람과 진동을 고려한 항공기 탑재 AESA 레이다 성능 평가용 운동 모델링 및 시뮬레이션)

  • Lee, Donguk;Im, Jaehan;Lee, Haemin;Jung, Youngkwang;Jeong, Jaehyeon;Shin, Jong-Hwan;Lee, Sungwon;Park, June Hyune;Ahn, Jaemyung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.48 no.11
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    • pp.903-910
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    • 2020
  • This paper introduces a simulator to assess the impacts of the wind and the airframe vibration on the performance of the Active Electronically Scanned Array (AESA) radar mounted in an aircraft. The AESA radar is mounted on the nose cone of an aircraft, and vibration occurs due to the drag force. This vibration affects the behavior of the AESA radar and can cause phase errors in signal. The simulator adopts the geometric model for nose cone, the mathematical models on the rigid-body dynamics of the aircraft, the average/turbulent winds, and the mode/ambient vibrations to compute the position and the attitude of the radar accurately. Numerical studies reflecting a set of test scenarios were conducted to demonstrate the effectiveness of the developed simulator.

Performance Analysis of an Integrated Navigation of an Airborne AESA Radar (항공기 탑재 AESA 레이다의 통합 항법 성능 분석 연구)

  • Lee, Dong-Yeon;Kwon, Hyeokjoon;Lee, Donguk;Lee, Haemin;Jung, Youngkwang;Jeong, Jaehyeon;Park, Sanggyu;Lee, Sungwon;Park, June Hyune;Tahk, Min-Jea;Bang, Hyochoong;Ahn, Jaemyung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.4
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    • pp.281-290
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    • 2021
  • For successful operations of an airborne Active Electronically-Scanned Array (AESA) radar, which has various advantages over traditional radar systems, accurate and robust navigation is critical. This paper discusses a study on the performance analysis of an integrated navigation based on the Embedded GPS/INS (EGI) system for an aircraft equipped with an AESA radar. The models for generating the inputs for the GPS/IMU are developed. A navigation filter for a loosely-coupled GPS/IMU system is constructed. Overall navigation performance assessment procedure using a six degree of freedom aircraft simulator - along with the GPS/IMU models and the navigation filter - is introduced. The steps of the performance analysis procedure are explained using a comprehensive case study.

Resource Allocation for Performance Optimization of Interleaved Mode in Airborne AESA Radar (항공기탑재 AESA 레이다의 동시운용모드 성능 최적화를 위한 자원 할당)

  • Yong-min Kim;Ji-eun Roh;Jin-Ju Won
    • Journal of Advanced Navigation Technology
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    • v.27 no.5
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    • pp.540-545
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    • 2023
  • AESA radar is able to instantaneously and adaptively position and control the beam, and this enables to have interleaved mode in modern airborne AESA radar which can maximize situational awareness capability. Interleaved mode provides two or more modes simultaneously, such as Air to Air mode and Sea Surface mode by time sharing technique. In this interleaved mode, performance degradation is inevitable, compared with single mode operation, and effective resource allocation is the key component for the success of interleaved mode. In this paper, we identified performance evaluation items for each mode to analyze interleaved mode performance and proposed effective resource allocation methodology to achieve graceful performance degradation of each mode, focusing on detection range. We also proposed beam scheduling techniques for interleaved mode.

Verification of Airborne Radar's Search Pattern Stabilization Capability Using SIL Environment (시스템 통합 시험 환경을 이용한 항공기 탑재 레이다의 탐색 패턴 안정화 기능 검증)

  • Ji-Eun Roh;Yong-Kil Kwak;Jin-Ju Won;Won-Jin Lee
    • Journal of Advanced Navigation Technology
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    • v.28 no.2
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    • pp.178-184
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    • 2024
  • The radar installed on an aircraft has various operating modes depending on tactical purposes, allowing for the configuration of search areas according to each mode's operational objectives. active electronically scanned array (AESA) radar emits search beams sequentially according to a predefined search beam grid within the designated search area specified by the pilot to detect targets within it. It is crucial that the radar can stably search the area designated by the pilot for target detection, even as the aircraft's attitude changes. This paper focuses on stabilizing the search pattern in the air-to-air operational mode of aircraft-mounted radar to ensure stable target detection during roll and pitch maneuvers of the aircraft. The paper demonstrates its performance by simulating aircraft maneuvers and targets in a system integration laboratory (SIL) test environment.

Implementation of AESA Radar Integration Analysis System by using Heterogeneous Media

  • Min-Jung Kang
    • Journal of the Korea Society of Computer and Information
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    • v.29 no.3
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    • pp.117-125
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    • 2024
  • In this paper, implement and propose an Active Electronically Scanned Array (AESA) radar integration analysis system which specialized for radar development by using heterogeneous media. Most analysis systems are used to analyze and improve the cause of defects, so they help the test easier. However, previous log analysis systems that operate only based on text are not intuitive and difficult to find the information user want at once if there is a lot of log information. so when an equipment defect occurs, there are limitations in analyzing the cause of defect. Therefore, the analysis system in this paper utilizes heterogeneous media. The media defined in this paper refers to recording text-based data, displaying data as image or video and visualizing data. The proposed analysis system classifies and stores data that transmitted and received between radar devices, radar target detection and Tracking algorithm data, etc. also displays and visualizes radar operation results and equipment defect information in real time. With this analysis system, it can quickly provide information what user want and assistance in developing high quality radar.