• Defense and Technology
• /
• no.9 s.127
• /
• pp.50-59
• /
• 1989

초기에 전차의 개발은 추진기관, 장갑, 탄약면에서 이루어졌었다. 그러나 고급 전자기술의 발달에 따라 특히 광학전자장비분야에 중점이 두어지기 시작하였다. 출력의 증가를 가져오는 엔진의 개발과 복합재료는 기동성과 방호력을 증대시켰다. 무장 역시 사정거리와 정확도에서 크게 개선되어왔다

• Defense and Technology
• /
• no.1 s.179
• /
• pp.52-61
• /
• 1994

곡사포탄은 적의 종심공격, 대포병사격, 적 전투차량 제압, 보병부대의 일반지원 등의 임무를 효율적으로 수행하기 위해 사거리 연장, 정확도 증대 및 위력증대의 3가지 목표를 극대화하는 방향으로 발전되어 왔다.

• Proceedings of the Acoustical Society of Korea Conference
• /
• spring
• /
• pp.177-180
• /
• 2000

소나 시스템에서는 신호 대 잡음비의 향상, 표적의 방위탐지 및 위치 데이터 산출, 간섭신호 제거 등을 위하여 지향성 빔을 만들어 사용한다. 본 논문에서는 선형으로 배열된 센서에서 각 센서쌍들에 대한 상호상관 행렬을 이용한 SCCBF(Spatial Cross Correlation Beamformer) 알고리즘을 제안하였다 이상적인 조건하에서 제안된 SCCBF는 CBF(Conventional Beamformer)에 비해 3dB의 Array Gain을 갖는 것을 이론적으로 검증하고 표적의 탐지 방위정확도를 나타내는 빔폭(Beam Width)이 CBF 보다 0.5배정도가 됨을 검증하고 모의실험을 통하여 이를 입증하였다.

• Journal of the Korean Society of Surveying, Geodesy, Photogrammetry and Cartography
• /
• v.22 no.4
• /
• pp.411-418
• /
• 2004

This paper is the study about a method for determining the azimuth of a baseline by measuring the apparent direction of the Sun. It is simple to realize this method, as it requires, in addition to the apparent direction of the Sun already measured, the observation time and the latitude and the longitude of the survey point. Comparing the azimuths determined by this method and those determined by the PDGPS(Post Processed Differential GPS) on 3 different baselines, the differences(PDGPS - this method) between the azimuths determined by two methods were -13", +45" and +24" respectively. It can be an effective and rapid tool in cases that require the accuracy lower than 1 arc-min.than 1 arc-min.

• The Journal of the Acoustical Society of Korea
• /
• v.20 no.2
• /
• pp.86-92
• /
• 2001

Various array processing techniques to identify the noise source position or bearing have been developed. Typical array processing techniques which are based on time delay between received signals at two sensors, are classified as conventional beamforming, correlation function and NAH (Near-Field Acoustic Holography) techniques which have their own characteristics with respect to application field and signal processing method. In this study, correlation function technique which could be applied for broadband noise source detection, is adopted and the effective detection technique is proposed considering the effects of source bandwidth and measurement noise correlation of noise sources. The validity of the Proposed technique is evaluated using the 3-dimensional nonlinear any which does not give 3-dimensional Position or bearing ambiguity

• Journal of Navigation and Port Research
• /
• v.41 no.4
• /
• pp.189-194
• /
• 2017

The Moving Search Radar System (MSRS) monitors sea areas by moving along the coast. Since the radar is initially aligned to the front of the vehicle, it is important to know the changes in the heading azimuth of the vehicle to quickly acquire the target azimuth from the radar after the MSRS has moved. The heading azimuth can be obtained using the gyro compass, the GPS compass or the electronic compass. The electronic compass is suitable for MSRS requiring fast maneuverability due to its small volume, short stabilization time and low price. However, using a geomagnetic sensor may result in an error due to the surrounding magnetic field. Errors can make early automatic tracking of the satellites difficult and can reduce the radar detection accuracy. Therefore, this paper proposes a method to automatically compensate for the error reflecting the correction value on the radar obtained by comparing the reference azimuth calculated by solving the geodesic inverse problem using two coordinates between the radar and the geostationary satellite with the actually-directed azimuth angle of the satellite antenna. The feasibility and convenience of the proposed method were verified by applying it to the MSRS in the field.

• Defense and Technology
• /
• no.8 s.222
• /
• pp.78-91
• /
• 1997

서구 각국은 군의 현대화와 효율성을 제고하기 위해 재래식 탄약에 센서, 전자/통신 및 탄두기술 등과 같은 첨단 기술을 도입, 적용하여 정확도 향상, 사거리 및 탄의 위력을 증대시키고 소량의 탄으로 대량 살상보다는 장갑표적 등과 같은 특정표적을 선별 제압 함으로써 전장에서의 우위를 확보하고자 하고 있다.

• Defense and Technology
• /
• no.10 s.152
• /
• pp.76-79
• /
• 1991

탐색기는 호밍유도탄에 사용되는 핵심 유도장치로서 저가의 전술유도탄에서부터 고가의 전략유도탄용에 이르기까지 여러 다른 목표와 사양으로 개발되고 있으며, 유도 무기체계의 경제성, 정확도의 개선, 명중률의 향상을 위해 설계요구조건이 더욱 다양화되고 있는 추세이다. 여기에서는 탐색기의 주요 연구분야 설계의 요구조건과 절차, 핵심 소요기술을 소개하기로 한다

• The Journal of Korean Institute of Electromagnetic Engineering and Science
• /
• v.27 no.8
• /
• pp.693-700
• /
• 2016

In this paper, it is represented that equations for design of linear interferometer antenna when the 3 dB beamwidth is only region of interest. Using the equations, relationships between angle measurement ambiguity and element antenna spacings are described. And then, operating frequency, angle measurement accuracy, beamwidth, correct measurement probability are calculated for five antennas interferometer to measure azimuth and elevation angle. The interferometer antenna was designed and fabricated using the calculated parameters. The angle measurement accuracy were $0.01^{\circ}$ and $0.016^{\circ}$ for azimuth and elevation axes with 99 % probability of doing measurements correctly which means that ambiguous solution did not occur more than 1 % of the time. These results validated the equations and design procedures.

• The Journal of the Acoustical Society of Korea
• /
• v.36 no.3
• /
• pp.218-227
• /
• 2017

In this paper, an algorithm to calculate both bearing and distance error for target detection and localization is proposed using the Cramer Rao lower bound to estimate the minium variance of their error in DOA (Direction Of Arrival) estimation. The performance of arrays in detection and localization depends on the accuracy of DOA, which is affected by a variation of SNR (Signal to Noise Ratio). The SNR is determined by sonar parameters such as a SL (Source Level), TL (Transmission Loss), NL (Noise Level), array shape and beam steering angle. For verification of the suggested method, a Monte Carlo simulation was performed to probabilistically calculate the bearing and distance error according to the SNR which varies with the relative position of the target in space and noise level.