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Concept Design of Angular Deviation and Development of Measurement System for Transparency in Aircraft

항공기 투명체의 편각개념 설계 및 측정 시스템 개발

  • 문태상 (국방기술품질원 사천센터 2팀) ;
  • 우성조 (한국항공우주산업(주) 세부계통팀) ;
  • 권성일 (한국화이바(주) 특수사업부 항공팀) ;
  • 류광열 (부산대학교 산업공학과)
  • Received : 2010.07.06
  • Accepted : 2010.10.29
  • Published : 2010.11.01

Abstract

Angular Deviation(AD) on transparency applied to TA-50 Aircraft deteriorates armament system's accuracy because it makes a difference in between actual and theoretical targets. In order to increase accuracy, therefore, TA-50 Aircraft measures AD on transparency and provide the measured values for the integrated mission display computer as a type of AD coefficients. This makes AD revised so that pilots can accurately see the actual target on their head-up display. In order to implement such mechanism into a real field, we develop a new device and system automatically measuring AD for the first time. We also deal with basic concept including AD induction formula as well as operating systems. As a consequence of testing the accuracy and precision for verifying reliability of the system, we got satisfactory results. In specific, the accuracy was within the resultant criterion of 1%. The precision was also satisfied with respect to the whole criteria. The system developed through this research is qualified as a military standard equipment for transparency of the canopy.

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