• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.27 no.12
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• pp.1097-1104
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• 2016

The infrared camera is difficult to satisfy the RE-102 specification of Mil-Std-461. Especially, in the case of UAV electronics, shielded cable is not used, so it is difficult to meet the electromagnetic compatibility standard. In the RE-102 test of the IR camera for UAV, radiated noise exceeding 30 dBuV/m was observed in the range of 50 MHz to 200 MHz. As a result of pcb em scan, peak noise which caused by the harmonic frequency of the digital control signal clock was observed. Radiated noise was reduced by up to 22.9 dBuV/m by applying the spread spectrum clock generator(SSCG) with 3 % down spreading method to the camera control clock.

• Aerospace Engineering and Technology
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• v.10 no.2
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• pp.82-86
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• 2011

This paper presents an RF Electric field assessment at 2.290 [GHz] inside launcher PROTON M/Breeze M long fairings, produced by COMS TM. COMS intentional RE due to TM ON under fairing has been assessed considering PROTON M / BREEZE M fairing characteristics. As fairings of all launchers present similar sizes, a similar E-field level under fairing is expected for the other launchers. As a result, the RE level under faring is compliant with COMS RS limits, but is not compliant with RS requirements of the launcher PROTON M/Breeze M.

• Journal of Advanced Navigation Technology
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• v.22 no.2
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• pp.105-110
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• 2018

The North Korea nuclear issue is now posing a serious security threat to the Korea and Northeast Asia. Accordingly, the South Korean military is pushing for the introduction of long-range air-to-surface flights and the development of domestic nuclear facilities that can precisely hit North Korea headquarters building and nuclear facility even hundreds of kilometers above the border. In this paper, we removed the cable braid for securing the weight of the missile among several design elements for long-range air-to-surface missile development and estimated and analyzed the resulting performance. The possibility of braid removal was analyzed in terms of crosstalk inside the cable and CS114, RE101 of MIL-STD-461F.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.12
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• pp.1207-1215
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• 2008

Satellite generates a complex electromagnetic noise by conducted and radiated coupling effect of the various electrical instruments. This noise may cause serious problems on the satellite system. To minimize the electromagnetic coupling effects and maintain the system safety margin, system noise reduction technique should be applied from the beginning of the system design. The COMS system is evaluated by measuring the conducted noise on system electrical power leads at PSR(Power Supply Regulator) and verifying a 6 dB system safety margin under the complex noise environment with current injection. The radiated noise due to the complex transmit antenna configuration is evaluated by integrating all unit-level RE measurement results, and the RF compatibility between spacecraft and launch vehicle is analyzed with the above estimations. This paper describes the COMS EMC compatibility analysis with respect to each unit level EMC test results, and RF compatibility analysis between spacecraft and launch vehicle. The analyzed results will be reflected on FM(Flight Model) EMC test.

• Proceedings of the KIEE Conference
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• 2009.07a
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• pp.1576_1576
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• 2009

We present the design of an EMI filter to mitigate the electrical noise from the power supply over a broadband of a few tens of KHz to 18GHz. Admitting that our approach is not apart from the standard technology of EMI filter, it is worth checking out how we can implement the filter that meets the challenging spec. on band of operation. The function of the EMI filter is well-depicted by its performance on the CE(Conducted Emission) and RE(Radiated Emission) suppression through tests which convince us of its application to power supplies of land, water and flying vehicles.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2018.05a
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• pp.404-407
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• 2018

- A car is a means of transporting passengers or cargo on the ground by transmitting power from the engine to the wheels. In the past, automobiles started from internal combustion engines have recently been introduced with hybrid electric vehicles and pure electric vehicles. As a result, the deployment of high-tech electrical and electronic products is inevitably increased due to the development of technology and stability of various parts, resulting in a more complicated and diversified electromagnetic environment. CISPR 25 is conducting research on the test method for electromagnetic noise. In order to analyze the noise pattern according to the GND condition required in the radiation emission test, various conditions are applied for comparison. 2 Page - General characteristics of EMI chambers, techniques for testing and measuring equipmen 3 Page - RE test : Analysis of Noise due to Ground Strap Change when Sample is in Center, Analysis of Noise due to Ground Strap Changes when the Sample is not in the Center.

• Proceedings of the KIEE Conference
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• 2005.07c
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• pp.2115-2117
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• 2005

회전기기인 고압 전동기 및 발전기의 고정자권선에서 나타나는 운전중 부분방전 진단을 위한 방법의 하나로 비접촉식 센서를 이용한 부분방전 측정에 관한 연구가 최근 들어 활발히 진행되고 있다. 그러나 이들 권선에서 나타나는 부분방전의 방사특성에 대하여 정확한 측정이 국내에서 체계적으로 검토된 실적이 없는 실정이다. 본 논문에서는 회전기 고정자권선의 부분방전 현상을 측정하는데 이용될 비접촉식 부분방전 진단센서를 개발함에 있어서 필요한 측정 주파수대역을 선정하는데 이용하고자, 여러 종류의 고정자 권선을 대상으로 전압을 인가하여 발생되는 부분방전의 펄스의 방사특성 및 잡음특성을 실험실적으로 측정하여 고찰하였다.

• Bulletin of the Korean Space Science Society
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• 2003.10a
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• pp.106-106
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• 2003

인공위성의 전기적 호환성 해석은 인공위성의 각 유닛들에서 발생할 수 있는 잡음이 인공위성의 정상 동작에 미치는 영향을 분석하고 그 영향을 최소로 만들 수 있는 방안을 연구하기 위해 필요하다. 본 논문에서는 인공위성의 탑제컴퓨터와 탑제체 간의 인터페이스에서 전기 신호의 호환성 해석, Harness의 호환성 해석 그리고 radiation 해석이 이루어졌다. 인공위성의 탑제컴퓨터와 탑제체 간의 인터페이스에서 전기 신호의 호환성 해석은 전기 신호의 전압 레벨이 전압 히스테리시스의 경계 영역에서 충분한 여유를 가지고 있는지 판단하기 위해 필요하다. 전기 신호에 충분한 여유분이 없는 경우 여유분을 증가시키기 위한 방법이 제안되었으며 제안된 방법에 의해 인터페이스의 올바른 동작에 충분한 여유분이 생겼음이 시뮬레이션 결과에 나타났다. Harness의 호환성 해석은 다목적실용위성 2호에 사용된 Harness에 대한 conductive epoxy potting의 전도도를 검증하기 위해 이루어졌다. 본 논문에서는 전송 임피던스 측정 방법을 이용하여 epoxy potting의 전도성이 모든 주파수 영역에서 인공위성의 요구사항에 만족함을 보여준다. Radiation 해석은 인공위성 시스템의 radiated emission(RE)을 추정하고 S-band 수신기와 GPS 안테나와 같은 수신단에 대한 상호간섭에 의한 위험도를 분석하기 위해 필요하다. RF 수신기의 수신 대역에서 발생한 잡음의 영향으로 신호대잡음비가 허용수치이하로 감소하여 위성 명령을 수신하는 동작에 지장을 초래할 수 있다. 본 논문에서는 RF 수신단에 가장 큰 영향을 미칠 것으로 예상되는 star tracker의 RE test 결과를 분석하여 test 결과가 GPS 수신기와 S-band 수신기의 각각의 성능에 적합한지 해석하였다. 또한 solar array regulator의 스윗칭에 의해 발생되는 radiation이 위성 구조체에 미치는 영향을 해석하고 시뮬레이션 하였다.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.19 no.2
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• pp.263-270
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• 2008

In this paper, we investigated EMI(electromagnetic interference) reduction by conductor connection, which was used for fixing and electrical grounding between frames. Conductor connects two frames and then it provides the decrease of return path of signal current. To prove the effect of conductor, we measured/simulated the RE(radiated emission) with/without conductors between the two frames. From the measured/simulated results, we observed that EMI decreased about 1$\sim$10 dB at the frequency range of 30 MHz to 1 GHz. VNA(vector network analyzer) was used to measure the S parameters and the RE was measured in a 3 m anechoic chamber. The simulated and measured results are compared and discussed.