• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2003년도 ICCAS
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• pp.2641-2647
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• 2003

Conventional DLLs estimate the delay times of satellite signals individually and feed back these measurements to the VCO independently. But VDLL estimates delay times and user position directly and then estimate the feedback term for VCO using the estimated position changes. In this process, input measurements are treated as vectors and these vectors are used for navigation. First advantage of VDLL is that noise is reduced in all of the tracking channels making them less likely to enter the nonlinear region and fall below threshold. Second is that VDLL can operate successfully when the conventional independent parallel DLL approach fails completely. It means that VDLL receiver can get enough total signal power to track successfully to obtain accurate position estimates under the same conditions where the signal strength from each individual satellite is so low or week that none of the individual scalar DLL can remain in lock when operating independently. To operate VDLL successfully, it needs to know the initial user dynamics and position and prevents total system from the divergence. The suggested integration method is to use the inertial navigation system to provide initial dynamics for VDLL and to maintain total system stable. We designed the GPS/INS integrated navigation system. This new type of integrated system contained the vector pseudorange format generation block, VDLL signal processing block, position estimation block and the conversion block from position change to delay time feedback term aided by INS.

• 대한토목학회논문집
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• 제29권1D호
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• pp.135-143
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• 2009

GPS 반송파를 사용하는 GPS/INS 통합 측위 기술은 서로가 가지는 기술적 한계를 상호 극복하여 그 성능을 최대화 할 수 있어 측량과 항법의 다양한 분야에 활용되고 있다. 그러나 GPS/INS 통합 측위을 통하여 수 센티미터의 정확도를 확보하기 위해서는 기준국과 이동국 수신기 사이의 간격이 10~20Km 이내로 제한되어야 하는 단점을 가지고 있으며 이는 두 시스템 관측데이터를 통합 처리하더라도 그 정확도는 여전히 GPS 위성궤도 오차, 전리층 영향 그리고 대류권 지연과 같은 기선장에 따른 오차의 영향을 받기 때문이다. 이것은 3대 이상의 기준국 관측데이터를 사용하여 기선장에 따른 오차 보정량을 추정하여 이동국 관측데이터에서 그 영향을 최소화하여 극복 할 수 있다. 따라서 본 논문에서는 다중의 기준국 관측데이터를 사용하여 기선장에 따른 오차 보정량 결정을 위한 기준국 반송파 미지정수 결정, 칼만필터에 의한 기선장에 따른 오차 추정 그리고 기준국과 이동국의 기하관계에 의한 오차 보간을 통한 보정량 산출 알고리즘 제안하고 실제 관측데이터 처리를 통해 그 성능을 평가 하였다.

• 한국측량학회지
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• 제27권2호
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• pp.225-234
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• 2009

실시간 공중 자료획득 시스템은 긴급상황에서 DEM, 정사영상과 같은 공간정보를 실시간으로 생성하기 위해 빠른 자료 수집을 수행하는 시스템이다. 이러한 시스템에서 GPS와 INS는 플랫폼의 위치와 자세정보를 획득 하는데 중요한 역할을 한다. 그러므로 이번 연구에서는 실시간 공중 자료획득 시스템에 장착될 GPS/MEMS IMU 센서의 성능을 평가하였다. 그리고 시뮬레이션 데이터를 통하여 실시간 자료 수집에 더욱 적절한 GPS/INS 통합 알고리즘을 확인하였다. 정지 상태와 이동 상태에서의 GPS/MEMS IMU 센서 성능 평가 결과 각각 3$\sim$4m, 2$\sim$3m의 위치오차를 확인하였다. 또한 자기장 센서를 사용하는 Aerospace 모드에서 더 높은 정밀도의 자세 결과를 확인하였다. EKF와 UKF의 비교에서는 직선 뿐만 아니라 곡선에서도 많은 차이를 보이지 않았다. 하지만 계산 시간에서 EKF가 UKF에 비하여 약 25배 빠르므로 실시간 공중 자료획득 시스템의 GPS/INS 통합 알고리즘에는 EKF가 더욱 적합한 것으로 판단된다.

• 한국측량학회지
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• 제30권2호
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• pp.181-188
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• 2012

최근 항공측량분야에서 항측용 디지털카메라와 라이다 및 GPS/INS와 같은 센서들을 이용해 다양한 공간정보를 획득하고 있다. 또한 GPS/INS와 항측용 디지털카메라의 연계를 통한 Direct Georeferencing 기술이 널리 활용되고 있다. 하지만 여러 센서의 결합에 따른 센서검정(Sensor Calibration)을 실시해야 하는 문제점이 따른다. 특히, 통합센서의 Boresight Calibration은 GPS/INS 항공삼각측량 및 Direct-georeferencing을 사용하는 작업절차에서 중요한 요소이다. 이를 해결하기 위해 본 연구에서는 항공기용 센서의 검정을 위한 국가차원의 테스트베드를 세종시 부지에 설치하고 항공영상의 항공삼각측량에 의해 함께 사용되는 GPS와 INS 센서결합에 따른 정확한 검정을 수행하여 시스템 변수의 정의, 시스템적인 에러를 평가하고 Direct Georeferencing에 필요한 외부표정요소 직접결정을 위한 효율적인 방법의 조사와 통합된 센서의 정확도 평가를 수행하였다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2003년도 ICCAS
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• pp.990-994
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• 2003

When the low cost IMU is used, the result of the stationary self alignment is not suitable for navigation. In this paper, an in-motion alignment method is proposed to obtain an accurate initial attitude of a low cost IMU based GPS/INS integration system. To design Kalman filter for alignment, large heading error model is introduced. And then Kalman filter is designed to estimate initial attitude error as the indirect feedback filter. In order to assess performance of the alignment method, computer simulations are carried out. The simulation results show that initial attitude error rapidly reduces.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2002년도 Proceedings of International Symposium on Remote Sensing
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• pp.423-427
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• 2002

Contrary to the traditional text-based information, 4S(GIS,GNSS,SIIS,ITS) information can contribute to the citizen's welfare in upcoming era. Recently, GSIS(Geo-Spatial Information System) has been applied and stressed out in various fields. As analyzed the data from GSIS arena, the position information of objects and targets is crucial and critical. Therefore, several methods of getting and knowing position are proposed and developed. From this perspective, Position collection and processing are the heart of 4S technology. We develop 4S-Van that enables real-time acquisition of position and attribute information and accurate image data in remote site. In this study, the configuration of 4S-Van equipped with GPS, INS, CCD and eye-safe laser scanner is shown and the merits of DGPS/INS integration approach for geo-referencing is briefly discussed. The algorithm of DGPS/INS integration fur determination of six parameters of motion is eccential in the 4S-Van to avoid or simplify the complicated computation such as photogrammetric triangulation. 4S-Van has the application of Laser-Mobile Mapping System for three-dimensional data acquisition that merges the texture information from CCD camera. The technique is also applied in the fields of virtual reality, car navigation, computer games, planning and management, city transportation, mobile communication, etc.

• 제어로봇시스템학회논문지
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• 제13권1호
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• pp.72-78
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• 2007

Determination of the local vertical is not trivial for a moving vehicle and in general will require corrections for the Earth geophysical deflection. The vehicle's local vertical can be estimated by INS integration with initial alignment in SDINS(Strap Down INS) system. In general, the INS has drift error and it cause the performance degradation. In order to compensate the drift error, GPS/INS augmented system is widely used. And in the event that GPS is denied or unavailable, celestial navigation using star tracker can be a backup navigation system especially for the military purpose. In this celestial navigation system, the vehicle's position determination can be achieved using more than two star trackers, and the accuracy of position highly depends on accuracy of local vertical direction. Modern tilt sensors or accelerometers are sensitive to the direction of gravity to arc second(or better) precision. The local gravity provides the direction orthogonal to the geoid and, appropriately corrected, toward the center of the Earth. In this paper the relationship between direction of center of the Earth and actual gravity direction caused by geophysical deflection was analyzed by using precision orbit simulation program embedded the JGM-3 geoid model. And the result was verified and evaluated with mathematical gravity vector model derived from gravitational potential of the Earth. And also for application purpose, the performance variation of pure INS navigation system was analyzed by applying precise gravity model.

• 수산해양기술연구
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• 제42권2호
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• pp.97-103
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• 2006

The integrated navigation system(INS) for fishing boat which organized the marine radar, global positioning system(GPS) compass, automatic identification system(AIS), echo sounder, GPS and electronic nautical chart(ENC) was manufactured to reduce the marine accidents of fishing boats occurred frequently at coastal and offshore. The application possibility of INS for fishing boat was examined for basic experiments in the sea. Integration display of various information, such as other vessel's behavior, depth, own vessel's position etc. was done to help the operate user who understood the circumstance around own boat. Therefore, the system will be utilized as a useful equipment for safety voyage and fishing work on the fishing ground.

• 한국군사과학기술학회지
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• 제11권3호
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• pp.30-39
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• 2008

An artificial vision aided NDGPS/INS system has been developed and tested in the dynamic environment of ground and flight vehicles to evaluate the overall system performance. The results show the significant advantages in position accuracy and situation awareness. Accuracy meets the CAT-I precision approach and landing using NDGPS/INS integration. Also we confirm the proposed system is effective enough to improve flight safety by using artificial vision. The system design, software algorithm, and flight test results are presented in details.

• 제어로봇시스템학회논문지
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• 제8권12호
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• pp.1067-1075
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• 2002

The system error model for the compensation of the low-cost personal navigation system is derived and the error compensation method using GPS is also proposed. The walking navigation system (WNS) that calculates navigation information through walking detection has small error than INS, but the error also increases with time. In order to improve reliability of the system regardless of time, WNS is integrated with GPS. Since WNS is usually used in urban area, the blockage of CPS signal is frequently occurred. Therefore tightly coupled Kalman filter is used for the integration of WNS and GPS. In this paper, the system model for the design of tightly coupled Kかm filter is designed and measurement is linearized in consideration of moving distance error. It is shown by Monte Carlo simulation that the error is bounded even through the number of visible satellite is less than 4.