• Title/Summary/Keyword: 레이다 시뮬레이터

Search Result 38, Processing Time 0.025 seconds

A Study on the Radar Jamming Signal Simulator Design for the Test & Evaluation (시험평가용 레이다 재밍신호 시뮬레이터 설계 연구)

  • 최성린;이상훈;정회인
    • The Journal of Korean Institute of Communications and Information Sciences
    • /
    • v.27 no.2B
    • /
    • pp.160-169
    • /
    • 2002
  • While radar operator recognizes and tracks threat targets through the scope, it is essential to overcome the jamming signal that disturbs the normal operation of the radar. Therefore, to train operator and test the EW capability of the radar, this paper proposed the jamming signal simulation algorithm and design results to generate the deception jamming(range, velocity, angle deception and multiple false targets) and noise jamming signals(spot, barrage, swept spot and cover pulse noise). And also, the radar jamming signal simulator composed of the 6 constituents is developed on basis of the proposed algorithm and digital circuit design technique and confirmed the validity of the developed simulator by means of the test results to generate the various jamming signal.

Implementation of Airborne Multi-Function Radar Including Attitude Maneuvering (자세 기동을 고려한 항공기 탑재 다기능 레이다 통합 시뮬레이터 구현)

  • Ko, Jae-Youl;Park, Soon-Seo;Choi, Han-Lim;Ahn, Jae-Myung;Lee, Sung-Won;Lee, Dong-Hui;Yoon, Jung-Suk
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
    • /
    • v.28 no.3
    • /
    • pp.225-236
    • /
    • 2017
  • In this paper, a simulation test bed is presented which operates to provide full-scale simulation of airborne multi-function phased array radars. This simulation test bed provides a capability to evaluate the target tracking performance. To realize aircraft operation scenario, we developed 6DOF aircraft dynamics model which can generate trajectories and attitude of an aircraft. This procedure includes steady state flight trim search, autopilot design, and aircraft guidance command design. Also, the radar-environment integrated simulator includes target detection/measurement model and tracking filter. Developed simulator is validated by creating an air-to-air scenario.

Development of Automatic Terrain Following Simulator Using Digital Terrain Elevation Data (디지털 지형 고도 데이터를 이용한 자동 지형 추종 시뮬레이터 개발)

  • Jisu Lee;MunGyou Yoo;Hyunju Lee;Ki Hoon Song;Dong-Ik Cheon;Sangchul Lee
    • Journal of Aerospace System Engineering
    • /
    • v.18 no.1
    • /
    • pp.88-98
    • /
    • 2024
  • In this paper, an Automatic Terrain Following (ATF) Simulator using Digital Terrain Elevation Data (DTED) was proposed. This ATF Simulator consists of a Flight Simulator, a Radar Simulator, and a Terrain Following Computer (TFC) Simulator. DTED and radar scan data generated with DTED were used as the terrain information necessary for terrain following. The ATF Simulator provides three modes of operation: a passive mode that uses DTED, an active mode that uses radar scan data, and a hybrid mode that uses both. We developed an ATF Simulator that could reduce the cost and time required to develop a terrain following system using the LabVIEW development environment and the MATLAB App Designer development environment. It was verified by confirming that the ATF Simulator met all functional requirements.

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
    • /
    • v.48 no.11
    • /
    • pp.903-910
    • /
    • 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.

An Design and Implementation of a Simultor for Wireless factory automation Using Hand-Held Devices and Lego Blocks (핸드헬드 디바이스와 레고 블럭을 활용한 무선 자동화 공장 시뮬레이터 설계 및 구현)

  • 김홍규;문승진
    • Proceedings of the Korean Information Science Society Conference
    • /
    • 2004.10c
    • /
    • pp.442-444
    • /
    • 2004
  • 본 연구는 핸드헬드 디바이스와 레고 블럭을 이용하여 공장의 무인화와 실시간문제 탐지, 실시간 원격제어를 위한 무선기반의 자동화 공장을 위한 시뮬레이터 구현을 목표로 하였다. 이를 위해, PDA와 무선랜 기술을 이용하여 무선 공장 자동화모델을 시뮬레이션 하였으며, 원거리에서도 탐지 및 제어를 할 수 있으며 또한 발생되는 문제점을 미리 파악하고, 보다 정확한 공정관리 및 제어를 위해 시뮬레이션 모델을 설계 및 구현하였다. 향후, 이는 임베디드 리눅스뿐 아니라 WinCE 를 탑재한 휴대폰에서도 공정제어, 모니터링 등의 제어가 가능할 것으로 예측된다.

  • PDF

Development of a Simulator for RBF-Based Networks on Neuromorphic Chips (뉴로모픽 칩에서 운영되는 RBF 기반 네트워크 학습을 위한 시뮬레이터 개발)

  • Lee, Yeowool;Seo, Keyongeun;Choi, Daewoong;Ko, Jaejin;Lee, Sangyub;Lee, Jaekyu;Cho, Heyonjoong
    • KIPS Transactions on Computer and Communication Systems
    • /
    • v.8 no.11
    • /
    • pp.251-262
    • /
    • 2019
  • In this paper, we propose a simulator that provides various algorithms of RBF networks on neuromorphic chips. To develop algorithms based on neuromorphic chips, the disadvantages of using simulators are that it is difficult to test various types of algorithms, although time is fast. This proposed simulator can simulate four times more types of network architecture than existing simulators, and it provides an additional a two-layer structure algorithm in particular, unlike RBF networks provided by existing simulators. This two-layer architecture algorithm is configured to be utilized for multiple input data and compared to the existing RBF for performance analysis and validation of utilization. The analysis showed that the two-layer structure algorithm was more accurate than the existing RBF networks.

High Resolution Radar Model to Simulate Detection/Tracking Performance of Multi-Function Radar in War Game Simulator (통합 교전 시뮬레이터 환경에서 다기능 레이다 탐지/추적 성능 모의를 위한 고해상도 레이다 모델)

  • Rim, Jae-Won;Oh, Suhyun;Koh, Il-Suek
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
    • /
    • v.30 no.1
    • /
    • pp.70-78
    • /
    • 2019
  • In this paper, modeling of a high-resolution multi-function radar is proposed to simulate radar performance in a war game simulator, called AddSIM. To incorporate the multi-function radar model into the AddSIM, the modeling must comprise a component-based structure consisting of physics, logics, and information blocks. Therefore, we assign the RF hardware of a RADAR as the physic block, a controller as the logics block, and the RF specifications of the RADAR as the information block. Detailed modeling of the physics and logics blocks are addressed, and data structure is also presented on an engineering level. On a multi-target engaged scenario, the performance of the multi-function radar is numerically analyzed and its validation is examined.

A Design of Handling Quality Assessment Environment Based on FLIGHTLAB Model Using Legacy Simulator (레거시 시뮬레이터를 활용한 FLIGHTLAB 모델 기반의 조종성 평가 환경 설계 연구)

  • Yang, Chang Deok;Lee, Seung Deok;Cho, Hwan Heui;Jung, Dong Woo
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.44 no.6
    • /
    • pp.530-536
    • /
    • 2016
  • The handling quality simulator including high fidelity flight mechanics model is indispensable component to design and verify the flight control system. Korea Aerospace Industries, LTD. (KAI) has been performing LCH (Light Civil Helicopter) core technology development program regarding automatic flight control system (AFCS) software development. And KAI has been developing flight mechanics model using FLIGHTLAB to design and evaluate the AFCS flight control law. This paper presents the handling quality assessment environment development results through the combining FLIGHTLAB with a legacy simulator. And this paper details the FLIGHTLAB model, application development process and FLIGHTLAB interface design. The developed handling quality assessment environment has been demonstrated with the ADS-33E hover and pirouette MTE (Mission Task Element) maneuver simulation.

Multi-functional Fighter Radar Scheduling Method for Interleaved Mode Operation of Airborne and Ground Target (전투기탑재 다기능 레이다의 공대공 및 공대지 동시 운용 모드를 위한 스케줄링 기법)

  • Kim, Do-Un;Lee, Woo-Cheol;Choi, Han-Lim;Park, Joontae;Park, Junehyune;Seo, JeongJik
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.49 no.7
    • /
    • pp.581-588
    • /
    • 2021
  • This paper deals with a beam scheduling method in fighter interleaving mode. Not only the priority of tasks but also operational requirements that air-to-ground and air-to-air search tasks should be executed alternatively are established to maximize high-quality of situational awareness. We propose a real-time heuristic beam scheduling method that is advanced from WMDD to satisfies the requirements. The proposed scheduling method is implemented in a simulation environment resembling the task processing mechanism and measurement model of a radar. Performance improvement in terms of task delay time is observed.