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      비행체 진입각을 이용한 공중 폭발고도 계측 방법 = Measurement Method of Airburst Height Using the Approach Angle

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      https://www.riss.kr/link?id=A103422572

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      다국어 초록 (Multilingual Abstract)

      This paper proposes a method to measure the airburst height by utilizing a high speed camera. This method might be applied to the test of which flight target is alive after the burst. The proposed method consists of four main steps. The first step is to compute the impact point using the sea surface height. The second step is to compute the height of burst (HOB) by using the distance from the camera to the impact point. This could be different from the real explosion height. That is because the distance from the camera to the burst point is not the same as it from the camera to the impact point. Therefore, the third step is to calculate the approach angle of the flight target with respect to the installed camera. Then, the last step is to compensate the computed height by using the approach angle. The result of the proposed method is compared with it from the triangulation. In this paper, the HOB error is also analyzed regarding the approach angle difference. Based on this analysis, the camera position might be suggested for error reduction.
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      This paper proposes a method to measure the airburst height by utilizing a high speed camera. This method might be applied to the test of which flight target is alive after the burst. The proposed method consists of four main steps. The first step is ...

      This paper proposes a method to measure the airburst height by utilizing a high speed camera. This method might be applied to the test of which flight target is alive after the burst. The proposed method consists of four main steps. The first step is to compute the impact point using the sea surface height. The second step is to compute the height of burst (HOB) by using the distance from the camera to the impact point. This could be different from the real explosion height. That is because the distance from the camera to the burst point is not the same as it from the camera to the impact point. Therefore, the third step is to calculate the approach angle of the flight target with respect to the installed camera. Then, the last step is to compensate the computed height by using the approach angle. The result of the proposed method is compared with it from the triangulation. In this paper, the HOB error is also analyzed regarding the approach angle difference. Based on this analysis, the camera position might be suggested for error reduction.

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      참고문헌 (Reference)

      1 S. Yun, "Test and Analysis of Dispersion of DPICM Sub-Munition Using Triangulation Method" 5 : 94-107, 2007

      2 K Kang, "Measuring Technique for Height of Burst using Stereo-vision Recognition" 2 (2): 194-203, 1999

      3 J. Choi, "Measurement Technique for Sea Height of Burst Using Image Recognition" 2 (2): 76-83, 2000

      4 J. Kim, "Measurement Method of Flight Attitude Relating Flight Direction using High Speed Image" 2015

      5 Final Report on Test Operation Procedure, "Location of Impact of Airburst Positions" 1976

      6 J. Kim, "Flight Event Analysis Method using 3D Image Processing" 2016

      7 J. Kim, "Flight Attitude Measurement Technique of Weapon System using High Speed Image" 21 : 157-160, 2013

      8 J. Kang, "A Study on The Terminal Trajectory and Attitude Measurement Technique of Weapon System using High Speed Image" 163-166, 2010

      1 S. Yun, "Test and Analysis of Dispersion of DPICM Sub-Munition Using Triangulation Method" 5 : 94-107, 2007

      2 K Kang, "Measuring Technique for Height of Burst using Stereo-vision Recognition" 2 (2): 194-203, 1999

      3 J. Choi, "Measurement Technique for Sea Height of Burst Using Image Recognition" 2 (2): 76-83, 2000

      4 J. Kim, "Measurement Method of Flight Attitude Relating Flight Direction using High Speed Image" 2015

      5 Final Report on Test Operation Procedure, "Location of Impact of Airburst Positions" 1976

      6 J. Kim, "Flight Event Analysis Method using 3D Image Processing" 2016

      7 J. Kim, "Flight Attitude Measurement Technique of Weapon System using High Speed Image" 21 : 157-160, 2013

      8 J. Kang, "A Study on The Terminal Trajectory and Attitude Measurement Technique of Weapon System using High Speed Image" 163-166, 2010

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2026 평가예정 재인증평가 신청대상 (재인증)
      2020-01-01 평가 등재학술지 유지 (재인증) KCI등재
      2017-01-01 평가 등재학술지 유지 (계속평가) KCI등재
      2013-01-01 평가 등재 1차 FAIL (등재유지) KCI등재
      2010-01-01 평가 등재학술지 유지 (등재후보2차) KCI등재
      2007-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      2006-01-01 평가 등재후보 1차 PASS (등재후보1차) KCI등재후보
      2004-01-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.13 0.13 0.1
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.09 0.09 0.244 0.04
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