• 한국전자파학회논문지
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• 제17권8호
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• pp.773-787
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• 2006

비행체 탑재 레이다는 민군 겸용으로 기상에 관계없이 전천후로 비행체의 안전 항행, 임무 감시, 사격 통제, 충돌 회피, 이착륙 등 비행에 필수적인 항공 전자 장치이다. 본 논문에서는 헬기 탑재 다중 모드 X-밴드 펄스 도플러 레이다 시험 모델의 설계, 제작 및 비행 시험 결과를 제시한다. 레이다 시스템은 안테나부, 송수신부, 신호처리부와 전시부의 4개의 LRU로 구성되며, 개발 기술은 평판 슬롯 배열 안테나, TWTA 송신기, coherent I/Q detector, 디지털 펄스 압축, MTI, DSP 기반 도플러 FFT 필터, 적응 CFAR, 도플러 추정보상 기법, 비행 안정화 및 TWS 추적 처리기를 포함한다. 개발된 레이다 시스템의 설계 성능은 다양한 지상 고정 및 이동 시험과 헬기 탑재 비행 시험을 통하여 이동 비행체 이동 클러터 보상과 MTD 성능을 확인하였다.

• 한국군사과학기술학회지
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• 제17권1호
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• pp.90-95
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• 2014

The system design and the system performance analysis of 3D imaging laser radar system for the mapping purpose is addressed in this article. For the mapping, a push-bloom scanning method is utilized. The pulsed fiber laser with high pulse energy and high pulse repetition rate is used for the light source of laser radar system. The high sensitive linear mode InGaAs avalanche photo-diode is used for the laser receiver module. The time-of-flight of laser pulse from the laser to the receiver is calculated by using high speed FPGA based signal processing board. To reduce the walk error of laser pulse regardless of the intensity differences between pulses, the time of flight is measured from peak to peak of laser pulses. To get 3D image with a single pixel detector, Risley scanner which stirs the laser beam in an ellipsoidal pattern is used. The system laser energy budget characteristics is modeled using LADAR equation, from which the system performances such as the pulse detection probability, false alarm and etc. are analyzed and predicted. The test results of the system performances are acquired and compared with the predicted system performance. According to test results, all the system requirements are satisfied. The 3D image which was acquired by using the laser radar system is also presented in this article.

• 제어로봇시스템학회논문지
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• 제9권6호
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• pp.420-424
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• 2003

A new adaptive filter is proposed for an aided strapdown inertial navigation system(SDINS). The proposed filter can be used to effectively estimate the time-varying variance of the measurement noise. Then, the in-flight alignment for the radar aided SDINS is designed using the additive quatermion error model. Simulation results show that the proposed adaptive filter effectively improves the performance of the radar aided SDINS.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2013년도 추계학술대회 논문집
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• pp.416-421
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• 2013

In this paper, the design concept of the transport of defense equipment and processes were established. And the transport of large radar equipment design were investigated. Detailed design of moving equipment with reference to the U.S. military standard was performed.Damping system of the moving equipment by using a simulation designed to predict In order to minimize shock and vibration in the vehicle due to the irregular road surface is transmitted through. Analysis of the damping system was verified using the driving test.

• Journal of Advanced Marine Engineering and Technology
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• 제31권8호
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• pp.970-974
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• 2007

A mixer is a key component in the wireless communication systems. In this paper, we design a mixer which is used in a frequency modulated continuous wave(FMCW) radar system. The frequency sweep range of the radar is from 10 GHz to 11 GHz. The transmitted and received signals of the FMCW radar are applied to LO and RF ports of the mixer, respectively, but the frequency difference between the two signals, which is called "a beat frequency" is under a few KHz and depending on the distance to target. Thus the isolation between the LO and RF ports is very important factor to design this mixer. In this paper we propose a single balanced resistive mixer using GaAs MESFET for this application. We first design a single-ended type resistive mixer using a simulation tool, then design a balanced type to increase the LO-to-RF isolation of the mixer. We fabricated the mixer on the substrate of dielectric constant 10 and thickness 0.635 mm. The measured results show that the isolation and conversion loss of the mixer over the frequency band is 20dB and 10.5dB, respectively. The LO input power for operating the proposed mixer is +3dBm, which is lower than a general conventional mixer's LO power. The 1 dB compression point is 6dBm.

• Journal of electromagnetic engineering and science
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• 제9권3호
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• pp.118-123
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• 2009

This paper discusses the design and fabrication of a reference signal generator for a naval radar system, including the vibration environment test. The transmit signals of the S-band radar system are synthesized by the reference signal and the phase noise must lower than - 130 dBc/Hz at a 10 kHz offset frequency. To achieve this specification, the phase noise of the reference signal needs to be less than -165 dBc/Hz at a 10 kHz offset. For achieving very low phase noise performance by the reference signal generator, the phase locked loop technique is applied with a 10 Hz loop bandwidth. Also, this reference signal generator has ${\pm}0.35\;ppb$ short-term stability to minimize instant phase errors and high vibration sensitivity against a ship's shaking, unbalanced rotating of antennas and so on.

• 한국전자통신학회논문지
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• 제19권1호
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• pp.11-18
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• 2024

본 논문에서는 Chebyshev 다항식을 이용해서 차량용 근거리 레이다에서 사용하는 70GHz 대역 배열안테나를 최적 설계하였다. SRR(: Short Range Radar)에서는 근거리 내에 물표를 검출하면서 높은 FoV(: Field of View)를 확보하기 위한 빔폭과 낮은 SLL(: Side lobe level)을 가져야 한다. 최적 설계된 안테나는 76~81GHz에서 동작하며 안테나의 크기를 소형으로 하기 위해 12개의 패치를 직렬로 배열하여 구성하였고, 78GHz에서 SLL - 10dB이하, 안테나의 이득 15.4dB를 만족하고 빔폭 112.5o, 입력반사계수 -10dB이하의 성능을 갖는다. 본 논문에서는 Chebyshev 다항식을 이용해서 SRR을 위한 안테나의 설계를 진행하고 이를 기반으로 MRR과 LRR에 사용될 안테나 구조 설계를 위한 최적 설계법을 제시한다.

• 한국전자파학회논문지
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• 제20권5호
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• pp.460-470
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• 2009

본 논문에서는 포구 속도 측정을 위한 X-band CW(Continuous-Wave)도플러 레이더 구현에 관해 기술하였다. 본 논문에서의 레이더 구성품은 마이크로웨이브 송수신부, 신호 처리부, 전원부이며, 레이더의 운용 및 시험을 위하여 운용/분석 프로그램을 제작하였다. 레이더 송신 주파수는 중심 주파수 $f_0$에서 ${\pm}3\;MHz$ step의 5개 채널로 가변되며, 송신 출력은 25 dBm이다. 레이더의 최소 유효 수신 전력은 -117 dBm이다. 이러한 레이더의 기능은 비행 중인 탄자의 도플러 주파수를 획득하고 정밀 속도 점을 계산하여 최초 포구 이탈 순간의 속도를 추정한다. 레이더의 성능 평가는 현재 화포 시험에 적용되는 기준 장비를 사용하여 155 mm 화포 사격 시험을 통해 삼각대장착, 포신 장착의 두 가지 방법으로 비교 실시하였다. 기준 장비와의 비교 결과, 동등 성능임을 확인할 수 있었다.

• ETRI Journal
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• 제40권2호
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• pp.188-196
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• 2018

This paper presents a pulse radar system to detect drones based on a target fluctuation model, specifically the Swerling target model. Because drones are small atypical objects and are mainly composed of non-conducting materials, their radar cross-section value is low and fluctuating. Therefore, determining the target fluctuation model and applying a proper integration method are important. The proposed system is herein experimentally verified and the results are discussed. A prototype design of the pulse radar system is based on radar equations. It adopts three different pulse modes and a coherent pulse integration to ensure a high signal-to-noise ratio. Outdoor measurements are performed with a prototype radar system to detect Doppler frequencies from both the drone frame and blades. The results indicate that the drone frame and blades are detected within an instrumental maximum range. Additionally, the results show that the drone's frame and blades are close to the Swerling 3 and 4 target models, respectively. By the analysis of the Swerling target models, proper integration methods for detecting drones are verified and can thus contribute to increasing in detectability.

• International Journal of Aeronautical and Space Sciences
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• 제6권2호
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• pp.97-109
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• 2005

In this paper, the critical requirement for obstacle awareness and avoidance is assessed with the compliance of the equivalent level of safety regulation, and then the collision avoidance sensor system is presented with the key design parameters for the requirement of the smart unmanned aerial vehicle in low-altitude flight. Based on the assessment of various sensors, small-sized radar sensor is selected for the suitable candidate due to the real-time range and range-rate acquisition capability of the stationary and moving aircraft even under all-weather environments. Through the performance analysis for the system requirement, the conceptual design result of radar sensor model is proposed with the range detection probability and collision avoidance mode is established based on the time-to-collision, which is analyzed by collision scenario.