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진택성(Taek-Seong Jin),유구현(Gu-Hyun Ryu),강동석(Dong-Seok Kang),이철수(Cheol-Seol Lee),이규송(Kyu-Song Lee) 한국소음진동공학회 2015 한국소음진동공학회 학술대회논문집 Vol.2015 No.4
Avionics equipment mounted inside the aircraft is influenced by excitation which is transmitted through the aircraft structure. This excitation affect electronic performance and can cause deterrioration or failure. Therefore, Avionics equipment must be designed to perform proper function under vibration environment. In this paper, finite element model of the avionics was used to analyze dynamic characteristics of the avionics, via modal and random vibration analysis. The vibration level occurring in the avionics equipment was verified through resonance test and random vibration test.