Journal of Aerospace System Engineering (항공우주시스템공학회지)

The Society for Aerospace System Engineering (항공우주시스템공학회)
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Random response analysis of Missile Guidance Structure by using Finite Element Method

유한요소 해석을 이용한 Missile Guidance Structure의 Random response analysis

  • Kim, Jaeki (Dept. of Mechanical and Aerospace Engineering, ERI, Gyeongsang National University) ;
  • Nam, Kwangsik (Dept. of Mechanical and Aerospace Engineering, ERI, Gyeongsang National University) ;
  • choi, Jinkyu (Dept. of Mechanical and Aerospace Engineering, ERI, Gyeongsang National University) ;
  • Choi, Homin (Dept. of Mechanical and Aerospace Engineering, ERI, Gyeongsang National University) ;
  • Zhao, Shang (Dept. of Mechanical and Aerospace Engineering, ERI, Gyeongsang National University) ;
  • Yeom, Sang Hun (FMI) ;
  • Lee, Seoksoon (Dept. of Mechanical and Aerospace Engineering, ERI, Gyeongsang National University)
  • 김재기 (국립경상대학교 기계항공공학부) ;
  • 남광식 (국립경상대학교 기계항공공학부) ;
  • 최진규 (국립경상대학교 기계항공공학부) ;
  • 최호민 (국립경상대학교 기계항공공학부) ;
  • 조상 (국립경상대학교 기계항공공학부) ;
  • 염상훈 ;
  • 이석순 (국립경상대학교 기계항공공학부)
  • Received : 2015.06.08
  • Accepted : 2015.07.28
  • Published : 2015.06.30
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Abstract

In the vibration test, Most of the test specifications is standardized methods of sinusoidal excitation. However, in accordance with the ability of the test equipment progress and developments of electronic technology, methods of random vibration test is standardized in the MIL standard. Therefore, in this study, we tried to analyze Missile Guidance Structure using a finite element analysis with ABAQUS 6.13 that is commercial program. First, Random response analysis is analyzed. Following analyzing the results, we wanted to find the model that is lightweight and resonance does not occur.

Keywords

References

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