• 한국군사과학기술학회지
• /
• 제13권4호
• /
• pp.561-568
• /
• 2010

Instrumentation radar in a test range has an important role to measure target's TSPI(time, space, position, information). It is well known that it tracks a target stably using a beacon mode. But it may fail to track a target in a certain region using a beacon mode. In this paper, we modeled a simple missile shape similar to ATCMS with two beacon antenna and analyzed an antenna radiation pattern using MLFMM(Multi Level Fast Multipole Method) method. Using the analyzed result of the radiation pattern of the antenna and the attitude data of target, we simulated beacon tracking performance of an instrumentation radar. As a result of simulation, we showed that an instrumentation radar may lose the target because it tracks a area of the beacon antenna pattern.

• 한국군사과학기술학회지
• /
• 제14권3호
• /
• pp.405-413
• /
• 2011

Defense Systems Test Center in ADD supports increasingly various missile test requirements such as higher altitude event, multi target operation and low-altitude, high velocity target tracking. In this paper, we have proposed the development of instrumentation radar tracking status simulator based on virtual reality. This simulator can predict the tracking status and risk of failure using several modeling algorithms. It consists of target model, radar model, environment model and several algorithms includes the multipath interference effects. Simulation results show that the predict tracking status and signal are similar to the test results of the live flight test. This simulator predicts and analyze all of the status and critical parameters such as the optimal site location, servo response, optimal flight trajectory, LOS(Line of Sight). This simulator provides the mission plan with a powerful M&S tool to rehearse and analyze instrumentation tracking radar measurement plan for live flight test at DSTC(Defense Systems Test Center).

• 한국군사과학기술학회지
• /
• 제9권2호
• /
• pp.118-126
• /
• 2006

As weapon systems are becoming advanced and intelligent, they are designed to have such events like ejecting sub-munitions. So it is continually requested to measure the event time and position exactly. We can measure the event time and position by analyzing the complex signal of the instrumentation radar in the time domain and can also obtain the spin rate of the target by analyzing the complex signal in the frequency domain.

• 한국항해항만학회:학술대회논문집
• /
• 한국항해항만학회 2019년도 춘계학술대회
• /
• pp.119-120
• /
• 2019

X-band 항해용 레이더를 이용한 파랑계측시스템의 파고계측 정확성 검증을 위해 울릉도 주변해역의 부이 유의파고값을 분석하여 결과의 타당성을 확보하였다. 특히 울릉도부이(해양기상부이), 울릉읍파고부이, 구암파고부이 및 혈암파고부이의 유의파고를 계절별로 분석하여 레이더식 파랑계측 결과와의 상관계수를 도출하고 분석하였다.

• 제어로봇시스템학회논문지
• /
• 제7권8호
• /
• pp.711-715
• /
• 2001

In this paper, an effective filter structure for filtering of target glint in tracking radar systems is used to improve the performance of CLOS(Command to Line-Of-Sight) guidance. The filter decouples range and angel channels to that it has a sound mathematical basis as well as computation efficiency as applied to the IMM algorithm. The effective filter structure in conjunction with CLOS guidance is tested by a series of simulation runs and it is shown to have superior performance compared with the other filter structures.

• 한국군사과학기술학회지
• /
• 제14권5호
• /
• pp.788-797
• /
• 2011

This paper analyzes the accuracy on the approach and landing of aircraft to an airport through comparison with airbase Precision Approach Radar and aircraft track data of DGPS equipped in aircraft. The proposed analysis result could be a basis for verifying the possibility that DGPS can be utilized in Airbase precision approach and landing. Position identification capability of widely used commercial DGPS is fairly accurate on latitude and longitude, while there is a slight error for being used in an airbase accurate approach and landing of Category I precision when it comes to altitude. Thus, we tested accuracy by analyzing actual flight track data of high performance aircraft to verify the accuracy of the airbase approach and landing using DGPS. Through the research, we developed instrumentation to compare PAR track data with DGPS track data, which can be used in reducing the number of PAR verification Flight utilizing it as a system measuring PAR accuracy at PAR installation phase.

• 지구물리와물리탐사
• /
• 제8권2호
• /
• pp.119-128
• /
• 2005

하천에서 발생하는 세굴 과정을 파악하기 위해서 교량 우물통 주변의 침식 그리고 퇴적 양상을 조사하는 것은 필수적이다. 지구물리탐사법은 하천 하상변화를 파악하는데 매우 효과적이며, 과거에 발생한 하상의 세굴 현상을 이해하는데 도움을 줄 수 있다. 본 연구에서는 비파괴 지구물리탐사법인 지하 투과 레이다(Ground Penetrating Radar, GPR)를 이용하여 2002년 6월과 2002년 10월에 한강 내의 교각 주변을 대상으로 홍수전$\cdot$후 세굴에 의한 하상 변화,세굴과 되메움의 범위 및 깊이, 그리고 하상 매질을 조사하였다. 자료획득에는 100 MHz와 400 MHe안테나를 이용한 GSSI SIR 2000 시스템이 사용되었다. 하천의 흐름방향으로 조사한 24개의 교각 사이와 5개 교각의 주위를 돌며 획득된 GPR영상이 비교 제시되었다. 적절한 현장탐사장비와 탐사 절차가 적용된 GPR탐사는 교각 및 교대 주변의 하천 수심과 하상 지질학적 구조를 결정하는데 효과적일 수 있다는 결론을 얻었다.

• 한국항행학회논문지
• /
• 제2권2호
• /
• pp.84-99
• /
• 1998

탄도탄 요격용 유도무기의 closed-loop 유도기법으로 종말유도의 효율성을 증대시키기 위해 산정된 비행자세 각으로 표적을 요격하기 위한 중기유도 법칙을 제시한다. 제시된 유도법칙은 잡음환경하에서의 비선형 레이더 측정치를 사용하는 확장칼만필터(EKF) 알고리즘을 사용하여 추정된 표적의 상태변수를 이용하고 표적의 운동을 간략화 하여 구한 추정된 표적의 위치를 기반으로 한다. 제시된 중기유도법칙의 3차원 공간으로의 확장에 대해서도 연구한다. 제시된 중기유도법칙을 적용하고, 종말유도법칙으로 비례항법유도(PNG)을 사용하는 일련의 시뮬레이션을 통해 유도성능을 확인한다.

• ETRI Journal
• /
• 제33권1호
• /
• pp.27-31
• /
• 2011

This paper addresses estimating the frequency of a cisoid in the presence of white Gaussian noise, which has numerous applications in communications, radar, sonar, and instrumentation and measurement. Due to the nonlinear nature of the frequency estimation problem, there is threshold effect, that is, large error estimates or outliers will occur at sufficiently low signal-to-noise ratio (SNR) conditions. Utilizing the ideas of averaging to increase SNR and weighted linear prediction, an optimal frequency estimator with smaller threshold SNR is developed. Computer simulations are included to compare its mean square error performance with that of the maximum likelihood (ML) estimator, improved weighted phase averager, generalized weighted linear predictor, and single weighted sample correlator as well as Cramer-Rao lower bound. In particular, with smaller computational requirement, the proposed estimator can achieve the same threshold and estimation performance of the ML method.

• 한국농업기계학회:학술대회논문집
• /
• 한국농업기계학회 1996년도 International Conference on Agricultural Machinery Engineering Proceedings
• /
• pp.569-581
• /
• 1996

A microcomputer -based data acquistion system was designed and developed at Michigan State University , USA to conduct field data studies. The system designed for the research carried out used an Apple IIe microcomputer for collecting data on-board the tractor. An AII3 Analog to Digital (A/D_ convertor was chosen to interface each analog signal to the microcomputer. A commercially available Dj TPM II was employed to display information such as an engine speed, ground speed, percent drive wheel slip , distance travelled and area covered per hour. The frequency output from the radar unit was channeled through a frequency to voltage (F/V) convertor , so that AII3 Analog to Digital (A/D) convertor could read it. The fuel consumption was measured using on EMCO pdp-1 fuel flow meter attached to the engine fuel line. The draft of the tillage and other drag equipment was determined using strain gages attached to the drawbar of the tractor. The system was developed to collect the draft and fuel requirements for various farm equipment different kind of soils.