Journal of Aerospace System Engineering (항공우주시스템공학회지)

The Society for Aerospace System Engineering (항공우주시스템공학회)
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A Study on the Establishment of Environmental Test Procedures for the UAV

무인항공기 운용 환경조건 시험절차 수립

  • Yun, Sanguk (The 7th R&D Institute, Agency for Defense Development)
  • 윤상욱 (국방과학연구소 제7기술연구본부)
  • Received : 2019.04.12
  • Accepted : 2019.05.19
  • Published : 2019.06.30
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Abstract

In this paper, we test procedures to demonstrate operating environmental conditions that can be exposed to UAV during its life-cycle are proposed. They are set up to be used in a large-sized climate chamber, one of the facilities of the Agency for Defense Development corresponding with the system requirements. The test steps and profile details were more specifically suggested for rainfall, humidity, and temperature (low-temperature storage and operation, high-temperature operation and solar radiation), and MIL-STD-810G w/Change-1-based.

본 논문에서는 무인항공기가 수명주기 동안 노출될 수 있는 운용 환경조건 입증을 위한 시험절차를 제안한다. 시험절차는 국방과학연구소 초대형 기후환경 챔버에서 시스템 요구조건을 입증할 수 있도록 수립되었다. 다양한 환경조건 중 비행체 단위에서 요구받는 강우, 습도 및 온도(저온 저장, 저온 운용, 고온 운용 및 일광(고온 저장)) 환경조건에 대하여 MIL-STD-810G w/Change 1을 기반으로 수립된 시험단계와 상세 프로파일에 대해 제안하였다.

Keywords

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Fig. 1 Rain Test Profile

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Fig. 2 Humidity Test Profile

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Fig. 3 Low Temperature Storage Test Profile

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Fig. 4 Low Temperature Operation Test Profile

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Fig. 5 High Temperature Operation Test Profile

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Fig. 6 Solar Radiation Test Profile

Table 1 Environmental Test Capabilities

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References

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