• Electronics and Telecommunications Trends
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• v.32 no.3
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• pp.98-106
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• 2017

GPS 등과 같은 위성항법 시스템은 정밀한 시각동기가 요구되는 동기식 이동통신망, 전력망, 금융망과 같은 분야와 사용자의 정밀한 위치를 요구하는 차량 내비게이션, 항공기 및 자동차, 측지 측량분야는 물론 향후 드론 및 자율주행 차량 등과 같은 다양한 응용분야에서 그 활용도가 증가될 것이다. 또한, 스마트폰에서는 기본적으로 위성항법 칩셋이 내장되어 사용자 위치를 제공하고 있다. 이렇듯 다양한 분야에서 활용되는 위성항법 수신 칩셋 또는 수신 시스템의 기능 및 성능을 다양한 환경에서 검증할 필요성이 대두되고 있다. 본고에서는 다양한 검증 환경을 제공할 수 있는 위성항법 신호생성기의 국외기술 동향을 살펴보고, 미래부 출연사업인 GNSS 전파교란 검증플랫폼 과제를 통해 개발된 GNSS 전파혼신 신호발생장치에서 확보한 실제 GPS 신호와 동기를 유지한 신호생성기술 개발 현황을 소개한다.

• Proceedings of the KIEE Conference
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• 2002.07d
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• pp.2105-2107
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• 2002

Geometry PIG 시스템은 배관의 상태 및 이상유무를 검사하여 그 결과를 저장하는 시스템으로 항법장치를 내장하고 있어 배관의 위치를 추정할 수 있다. PIG의 위치결정을 위해 후처리 보조 항법 알고리듬으로 비선형 스무딩 필터를 적용하고. 필터 측정치로 GPS를 이용한 위치기준점의 위치정보와 속도계를 이용한 속도정보를 사용하고, 특히 본 논문에서는 이들 정보 외에 Weld detector를 이용한 직선이동거리정보를 이용한 후처리 보조 항법 알고리듬을 PIG 시스템에 적용한다.

• IE interfaces
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• v.10 no.1
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• pp.145-154
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• 1997

In developing the HMI(Human-Machine Interface) evaluation system for the IVNS(In-Vehicle Navigation System), design guidelines and evaluation methods are the most crucial problems for its use and efficiency. As the part of this system, focused on the final product of the database, subjective mental workload assessment is seriously considered to evaluate the driver's own driving task using the IVNS. This paper suggests the methodology for the ergonomic assessment of the IVNS that corresponds to the subjective measurement of the driver's mental workload by rating his or her own driving task. For this approach, Revision of NASA-Task Load Index(RNASA-TLX) was developed which translated and revised the version of NASA-TLX that is generally accepted an efficient and powerful method for evaluating the in-vehicle information systems. To verify the RNASA-TLX, an experiment was conducted in a real road situation, because the result of the laboratory approach is uncertain and has the differences from the real road test.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.5
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• pp.74-80
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• 2006

GPS, which has been opened to the public since the 1980's, uses the C/A code time of arrival to estimate the position, and measures the carrier doppler frequency to estimate the velocity. In development from the 1990's, DGPS has improved position accuracy by eliminating common errors and CDGPS has achieved cm-level position accuracy using carrier phase. In this paper, a modified LSAST ambiguity resolution method for CDGPS is proposed to improve reliability and computational efficiency. Also the test results of cm level relative positioning of a moving vehicle using single frequency GPS receivers are compared to INS position. This research result can be widely used for the development of high precision INS, unmanned autonomous driving, survey and mapping, etc.

• Proceedings of the Korea Water Resources Association Conference
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• 2012.05a
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• pp.442-442
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• 2012

농업용저수지 수질측정 현황은 17,600여 개소 농업용저수지 중 농업용수 수질측정망 조사시설은 저수지 800개소이며, 농업용 호소로서 환경부 조사 시행 호소수질측정망시설 26개소(저수지 16개소, 담수호 10개소)를 포함한 826개소를 대상으로 농업용수 수질을 분석 평가하고 있다. 저수지 자율항법 자동수질측정을 위하여 개발한 운영시스템은 내용적측정 무인탐사선과의 연계운항 제어모듈 개발 및 저수지 수질측정을 위한 최적항로 운항모듈을 개발하였다. 자율항법 무인탐사선의 자동수질 측정을 위한 운항 제어 알고리즘 설계를 위하여 기존의 자율항법 탐사선의 운항 알고리즘과 수질자동 측정장치 제어 알고리즘을 분석하여 연계 제어모듈을 설계하고 프로그래밍 하였다. 운영과정은 선박운영 프로그램에서 수질모니터링 프로그램으로 Operation Start 명령을 전송하면 수질모니터링 프로그램에서 이 명령을 수신한 이후에 윈치제어 및 수질측정, 각 해당 수심에서 시료채수를 수행한 이후에 Opeartion End 신호를 선박운영 프로그램에 전송하면 다음 지점으로 이동할 수 있도록 하였다. 이를 통하여 효율적인 농업용저수지의 무인자동 수질측정 및 채수기술을 개발 제공하도록 하겠다.

• Journal of the Korea Institute of Military Science and Technology
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• v.24 no.6
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• pp.577-590
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• 2021

In this paper, we theoretically analyzed the self-alignment/navigation performance in the accelerometer resonance state generated by dither motion of ring laser gyroscope in LINS and verified it through simulation. As a result of analysis, it is confirmed that the amplitude of the accelerometer measurement amplified in the accelerometer resonance state is decreased in the process of sampling per the navigation calculation period and that frequency is changed by the aliasing effect too. It was also analysed that the attitude error in self-alignment is determined by the amplitude/frequency of the accelerometer measurement, the gain of the self-alignment loop, and the velocity and position error in the navigation is determined by the amplitude/frequency/phase error of the accelerometer measurement. This analysis and simulation results show that the self-alignment and navigation performance is not be degraded only when the amplification factor of the accelerometer measurement in the accelerometer resonance state is 3 or less

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.2
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• pp.128-136
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• 2011

An approach to improve the performance of SDINS and GPS integrated system for bank-to-turn flight vehicles is described. Then, it is shown through the simulation that a specific gyro misalignment error results in an increased heading error of SDINS. A new modelling method is presented herein for identifying of sensor and attitude error. The main advantage of the proposed method is that it not only estimates the gyro misalignment error of SDINS, but also improves estimate performance of heading error of SDINS in the presence of the gyro misalignments.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.20 no.2
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• pp.18-25
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• 2012

The availability of the GPS signal has been expanded greatly in the field of society overall through the development and construction of the GNSS(Global Navigation Satellite System). Furthermore, in the military, aviation and field of space, the GPS signal is applied widely through the combination of INS consisting of gyroscope and accelerometer, IMU, AHRS with the addition of magnetic sensor. Particularly, the performance of these equipments or sensors is very important with GPS and PAR(Precision Approach Radar) in the flight control of the aircraft. This paper deals with MATLAB simulation and ROLSO(Reduced Order Luenberger State Observer) design to reduce the load of system and realize the stable lateral direction approach control in an appropriate time for reduction of the horizontal error which is importantly considered while an aircraft lands instead of the FOLSO(Full Order Luenberger State Observer) using all measurement values. Consequently, ROLSO is expected to be used for the aircraft's attitude control in the aircraft landing causing the burden to the pilots.

• Journal of the Korean Institute of Intelligent Systems
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• v.21 no.6
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• pp.755-760
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• 2011

This paper presents a method for improving the positioning accuracy of the laser navigation. As a wireless navigation system, the laser navigation which is more flexible than a wired guidance system is used for the localization and control of an AGV(automatic guided vehicle). However, the laser navigation causes the large positioning error while the AGV turns or moves fast. To solve the problem, we propose the method for improving the positioning accuracy of the laser navigation using particle filter which has robust and reliable performance in non-linear/non-gaussian systems. For the experiment, we use the actual fork-type AGV. The AGV has a gyro, two encoders and a laser navigation. To verify the performance, the proposed method is compared with the laser navigation which is a product. In the experimental result, we verified that the proposed method could improve the positioning accuracy by approximately 66.5%.

• Defense and Technology
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• no.12 s.250
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• pp.36-45
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• 1999

우리는 천마의 개발 및 양산 이후에도 추가 연구개발 및 성능개량을 지속시켜 나가야 한다. 먼저 추적레이더의 S/W를 완전 국산화하고, 사격통제장치 기능을 최적화하고 방공 경보체계와의 연동능력을 보강해야 하며, 지상항법장치 등 지상장비 부수장치와 유도탄 잔종부품을 국산화하고 유도탄의 속도 및 기동력을 증대시키는 과제를 안고 있다.