• Title/Summary/Keyword: JDAM

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Application of MSAP to JDAM Separation from an F/A-18C Aircraft (MSAP을 이용한 F/A-18C로 부터 JDAM 분리 해석)

  • Lee Seungsoo
    • Journal of computational fluids engineering
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    • v.9 no.1
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    • pp.41-47
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    • 2004
  • A successful store separation analysis tool, MSAP(Multi-body Separation Analysis Program) has been applied to F/A-18C/JDAM CFD Challenge Ⅱ. The challenge was devised to challenge CFD community to use CFD methodologies to predict and match the trajectory of a JDAM MK-84 separating from F/A-l8C. Trajectory simulations for two flight conditions were performed. Comparison between computed and measured flight trajectories for both conditions shows a good agreement.

Application of MSAP to JDAM Separation from an F/A-l8C Aircraft (MSAP을 이용한 F/A-l8C로부터 JDAM 분리 해석)

  • Lee Seungsoo
    • 한국전산유체공학회:학술대회논문집
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    • 2003.08a
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    • pp.89-94
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    • 2003
  • A successful store separation analysis tool, MSAP(Multi-body Separation Analysis Program) has been applied to F/A-18C/JDAM CFD Challenge II. The challenge was devised to challenge CFD community to use CFD methodologies to predict and match the trajectory of a JDAM MK-84 separating from F/A-l8C. Trajectory simulations for two flight conditions were performed. Comparison between computed and measured flight trajectories for both conditions shows a good agreement.

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Dynamic Launch Zone Algorithm Using Machine Learning (머신러닝을 활용한 동적발사영역 산출 알고리즘)

  • You, Eun-Kyung;Bae, Chan-Gyu;Kim, Hyeock-Jin
    • Proceedings of the Korean Society of Computer Information Conference
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    • 2020.01a
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    • pp.35-36
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    • 2020
  • 본 연구는 TA-50 항공기 임무컴퓨터에서 JDAM을 가상으로 운용하는데 필요한 소프트웨어 개선 내용 중 가상 JDAM 무장 투하 구역 계산 방법을 제안한다. 이 연구에서 제안한 무장투하구역 알고리즘은 FA-50 JDAM DLZ에서 추출한 무장투하구역 입/출력값을 tensorflow를 사용하여 학습한 알고리즘이다. 이 연구를 통해 제안한 가상 JDAM DLZ 알고리즘을 사용할 경우 실제 무장을 장착하지 않은 항공기에서 가상으로 JDAM 무장 투하 구역 표시가 가능하고, 조종사는 가상의 JDAM DLZ를 참고하여 무장 투하 훈련을 수행할 수 있다.

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Implementation of JDAM virtual training function using machine learning

  • You, Eun-Kyung;Bae, Chan-Gyu;Kim, Hyeock-Jin
    • Journal of the Korea Society of Computer and Information
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    • v.25 no.11
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    • pp.9-16
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    • 2020
  • The TA-50 aircraft is conducting simulated training on various situations, including air-to-air and air-to-ground fire training, in preparation for air warfare. It is also used for pilot training before actual deployment. However, the TA-50 does not have the ability to operate smart weapon forces, limiting training. Therefore, the purpose of this study is to implement the TA-50 aircraft to enable virtual training of one of the smart weapons, the Point Direct Attack Munition (JDAM). First, JDAM functions implemented in FA-50 aircraft, a model similar to TA-50 aircraft, were analyzed. In addition, since functions implemented in FA-50 aircraft cannot be directly utilized by source code, algorithms were extracted using machine learning techniques(TensorFlow). The implementation of this function is expected to enable realistic training without actually having to be armed. Finally, based on the results of this study, we would like to propose ways to supplement the limitations of the research so that it can be implemented in the same way as it is.

Validation of Chimera Grid Method Applied to UMSAPv With Prediction of Carriage Load (장착하중 예측을 통한 UMSAPv에 적용된 중첩 격자 기법 검증)

  • Kang, SeonWook;Ahn, Kyehyun;Lee, Seungsoo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.50 no.10
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    • pp.669-676
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    • 2022
  • In this paper, the carriage load analyses of stores installed on aircraft are conducted to validate the chimera grid method applied to an unstructured CFD solver, UMSAPv. First, the chimera grid method of UMSAPv is verified for the well-known Eglin Wing/Pylon/Finned store problem. Next, an angle of attack sweep of F/A-18C clean configuration is conducted at a subsonic speed. The computed results are compared with the results of the previous study using MSAPv, a structured CFD solver, to show the validity of Umsapv. Finally, the carriage of F/A-18C JDAM is carried out with a chimera grid as well as a single block grid. The computed results are compared with other computational, experimental and the flight tests.

Analysis of Anti-jamming for GPS Guided Missile by GPS Reception Azimuth Control (GPS 수신 방위각 제어를 통한 GPS 유도무기 재밍대응 분석)

  • Choi, Chang-Mook
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.20 no.3
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    • pp.677-682
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    • 2016
  • Recently, because Global Positioning System (GPS) achieves accuracy for engagement of enemy targets, GPS guided weapons have a wide range of applications from land through sea to air. Especially, when GPS guided weapon is then launched, it reads current position and searches a course to the target. As we all know, because GPS signals are weak, these signals can be affected by interference. If jamming signal is strong enough, it can jam the receiver of GPS guided weapon. Therefore, anti-jamming technique is an important thing under these conditions. In this paper, the controlling azimuth angle was used to improve navigation performance of precision guided missile under jamming conditions. First of all, precision missiles by GPS positioning such as SLAM-ER and JDAM were investigated. Also, the azimuth cutoff angle of satellites for usable navigation under jamming signals was analyzed by experimental tests. As a result, we found that azimuth cutoff angle under 140 degree can help ensure continuous GPS reception under the missile guidance.

KF-16 Software Upgrade Cost Analysis (KF-16 항공기 SW성능향상사업 비용분석)

  • Min, Sung Ki;Lee, Cheol Woo;Dalton, Carl
    • Journal of the Korean Society of Systems Engineering
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    • v.2 no.1
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    • pp.18-23
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    • 2006
  • The purpose of this study and report is to provide, to the MND, an independent cost analysis of modernizing software of F-16 fighter fleets to support the use of several weapon system options, including JDAM, AIM-9X and HARM Targeting System etc. The study analyzed each options with software sizing, software cost, enabling hardware cost, flight test cost, system engineering cost, and 3 strategies. And the study proposed and analyzed some alternative strategies: strategy1 is to modernize software only within existing electronic processing capability; strategy2 is a full upgrade of weapons avionics with plug compatible electronics; strategy3 is an approach defined to mirror the USAF Common Configuration Implementation Approach (CCIP). The recommended alternative is strategy2.

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