• Aerospace Engineering and Technology
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• v.5 no.2
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• pp.102-107
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• 2006

In this study, the dynamic environment of satellite consists of excessive vibration at low frequency and irregular acceleration transferred by launch vehicle structure. Excessive vibration at low frequency is generally approximated by a sinusoidal wave from 100Hz to 200Hz and primarily used to preliminary design The random vibration is created by structural vibration due to the combustion of launch vehicle, separation stage and external aerodynamic noise. these are transferred to the adapter structure between satellite and launch vehicle through the structure of launch vehicle. random vibration is being specified for acceptance tests, screening tests, and qualification tests, because it has been shown that random vibration more closely represents the true environments in which the electronic equipment must operate.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2008.04a
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• pp.119-126
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• 2008

방위산업분야의 항공기용 전자장비는 신뢰성 설계를 위하여 MIL규격이나 실측된 PSD데이터를 이용하여 보수적으로 설계하는 것이 일반적이다. 하나의 프로젝트에서 개발되는 PCB는 수십 종에 이르고 그 장착위치나 설계변경이 병행되므로 PSD랜덤 진동해석의 대안으로 등가정적해석을 수행하게 된다. 등가정적해석결과의 보수성을 확인하기 위하여 PSD랜덤진동해석으로부터 추출된 정규분포를 갖는 각 방향 응력에 대해 Monte Carlo모의를 수행하여 결과를 비교분석하였다. 결론적으로 PSD랜덤진동 해석의 대안으로 등가정적해석결과의 유용성과 보수성을 통계적으로 비교하였고 실험을 통하여 결과의 타당성을 보였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.38 no.8
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• pp.798-805
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• 2010

Whole composite structure small class (150kg) satellite, STSAT-3, was initially developed in Korea. The structure does have aluminum frames that support the structure, and it is composed of only composite sandwich panels. A number of electronic boxes and mechanical apparatus will be shielded within the compartments built up by the composite panels. This study focused on the random vibration responses of the satellite. For this objective, vibration tests and analyses have been successfully performed with respect to STM (structure and thermal model) of the satellite. Additionally, through the experiment and theoretical analyses, the both results' accuracy was verified by comparison each other.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2010.10a
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• pp.372-373
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• 2010

• Journal of the Korea Academia-Industrial cooperation Society
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• v.22 no.3
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• pp.777-783
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• 2021

Aircraft are affected by various vibrations during maneuvering. These vibrations may have a fatal effect on the survival of aircraft in some cases, so the safety of components applied to the aircraft should be proven against various vibrations through random vibration analysis. In this study, the structural robustness of an external fuel tank and pylon for military aircraft was evaluated under random vibration conditions using commercial software, MSC Random. In the random vibration analysis, a frequency response analysis was performed by imposing a unit load on the boundary condition point, and then excitation was performed with a PSD profile. In this process, the required mode data was extracted through a modal analysis method. In addition, the random vibration profile specified in the US Defense Environment Standard was applied as random vibration conditions, and the PSD profile given in units of G's was converted into units of gravitational acceleration. As a result of the numerical analysis, we evaluated the structural robustness of the external fuel tank and pylon by identifying the safety margins of beam elements, shell elements, and solid elements in a numerical model for random vibration in the x, y, and z directions.

• Journal of KSNVE
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• v.8 no.4
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• pp.741-748
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• 1998

본 연구에서는 랜덤 기저가진을 받는 주 구조물과 여러 개의 부 구조물로 구성된 계의 응답특성을 분석하고 특히, 부 구조물의 응답분포에 관하여 연구하였다. 주 구조물의 응답이 최소가 되도록 설계변수를 최적화 할 경우, 부 구조물간의 응답분포가 균일하지 않음을 확인하고, 부 구조물간의 응답분포의 폭이 최소가 되는 진동수 비를 제안하였다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2011.04a
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• pp.837-842
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• 2011

• Journal of KSNVE
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• v.10 no.6
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• pp.971-976
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• 2000

High level random vibration environments induced while launching of spacecraft can damage sensitive electronic equipment, unless the equipment is properly packaged. Thus careful consideration on the launch environment, especially for high level random vibration, is required in the design stage of electronic equipment of spacecraft. This paper describes the development process of Solar Array Regulator for KOMPAT-2, which is designed and tested by Korean engineers. Both analytical and experimental techniques are introduced in this paper.

• Proceedings of the Korean Nuclear Society Conference
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• 1996.05d
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• pp.380-385
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• 1996

우리나라와 같이 강진의 발생이 거의 없는 지역에서, 가까운 장래에 예상되는 지진동 파형을 추정하는 기법으로서는 설계응답스펙트럼에 위상정보를 가미하는 모의지진동에 의한 작성방법을 흔히 사용하고 있으며, 이에 사용되는 위상스펙트럼의 특성을 랜덤으로 가정하는 경우가 대부분이다. 그러나 본 논문에서는 우리들이 일반적으로 랜덤으로 취급하는 위상스펙트럼에도 지진의 특성이 반영되어 있을 것이라는 가정하에 위상차분의 특성과 포락파형의 상관관계를 도출하고 위상차분을 고려한 모의지진동 작성방법을 제안하였다. 지진파형의 포락곡선을 확률분포로 사용하여 계산한 위상차분스펙트럼의 형상은 지진파형의 포락곡선과 거의 유사함을 확인하였고, 지금까지는 랜덤으로 취급한 위상스펙트럼에 물리적인 의미를 부여하는 계기가 되었다. 그러므로 앞으로 한반도에서 지진관측자료가 축적되어 한반도에서의 특징적인 위상차분스펙트럼이 정의된다면 우리나라의 지형조건이 고려된 진일보된 설계지진동을 작성할 수 있을 것이다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2002.11b
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• pp.886-889
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• 2002

In order to evaluate absorption coefficient, experimental works for normal and random incident absorption coefficient are made. An investigation for correlation between normal and random incident absorption was carried out by experiment and analysis. It appears that at the low frequencies, the random incident absorption is higher than the normal one, whileas at the high frequencies, the random incident absorption is decreased due to the effect of grazing incident components.