• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.11
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• pp.42-46
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• 2006

As an application of SDINS/GPS integration for its synergistic results, the SDINS alignments utilizing GPS carrier phase rate measurements. A measurement model of GPS carrier phase rate is derived in order to be used with SDINS alignment process. For in-flight alignment, the performance of the suggested SDINS/GPS integration method is analyzed using the covariance analysis and its results are confirmed by those of van test. Consequently, it is shown that all states of the SDINS integrated system by utilizing GPS carrier phase rate measurements can be estimated more efficiently than a general SDINS/GPS during in-flight alignment.

• Bulletin of the Korean Space Science Society
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• 2004.04a
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• pp.43-43
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• 2004

국제적인 시각비교를 위해 GPS를 이용하고 있으나, GPS 신호에는 위성까지의 거리정보뿐 아니라 위성시계, 대류층, 이온층, 다중경로 오차 등이 포함되어 있다. 그 중 이온층 지연시간을 측정하기 위해서는 Ll과 L2 반송파 신호로부터 얻어지는 P코드와 위상정보를 이용할 수 있다. 반송파 위상 정보는 P코드보다 해상도가 좋기 때문에 위상정보를 이용하게 되면 고정밀도의 이온층 지연시간을 얻게 된다. 이온층 지연시간을 통해 총전자수를 나타내는 TEC 값을 얻을 수 있는데, 관측지점으로부터 시간에 따라 가장 높은 고도의 위성을 선택하여 P코드와 반송파 위상 정보를 통한 이온층 총전자수를 파악하고 정밀도를 비교분석 하였다. (중략)

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.157.1-157.1
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• 2012

1990년대 제안된 RTK(Real-Time Kinematics)는 GNSS/GPS 반송파 위상(carrier phase) 관측값을 이용한 방식으로 cm 수준의 정확도를 실시간으로 산출할 수 있어 측지 측량 등 다양한 분야에서 활용되고 있다. 그러나 한 가지 중요한 단점은 이 방식을 사용하는 기준국과 사용자는 10~20km 이내에 존재해야만 빠르고 신뢰할 수 있는 해를 산출할 수 있다는 점이다. 이는 궤도오차, 대류층 및 전리층 오차에 공간 상관성(spatially correlated) 있기 때문인데, 사용자 주변을 둘러싼 다중 기준국들의 측정치를 조합하여 보상하거나 모델링하여 줄이는 방식인 다중 기준국 네트워크 기반의 RTK 알고리즘이 제안되어 사용되고 있다. 다중 기준국 네트워크 기반의 RTK 프로세스에서 기준국간 미지정수 결정은 전 과정의 핵심 프로세스라고 할 수 있으며, 관련되어 많은 기술들이 제안되고 연구되어 왔다. 특히, 1980년대 말부터 현재까지 후처리 기반으로 꾸준하게 연구되고 있는 Blewitt에 의해 전리층 제거 조합과 Wide-lane 반송파 위상 조합을 활용한 미지정수 검색 방법이 대표적이며 이후에도 Gao, Colombo등 다양한 연구자에 의해 활용되었다. 이 연구에서는 실시간으로 다중 기준국 반송파 미지정수를 결정하는 기술에 대한 연구를 수행하였다. L1, L2 관측값 조합으로 인한 관측값의 잡음 수준이 증가하는 영향을 피하기 위해 L1, L2 반송파 위상 및 의사거리를 그대로 관측값으로 사용하여 사용자 위치 및 속도, 기준국간 이중 차분된 전리층 지연 수직성분, 대류층 wet 지연 수직 성분, 이중 차분된 미지정수를 미지의 상태변수로 확장 칼만필터를 통해 직접적으로 추정하는 방식으로 미지정수의 실수해를 결정하였고, 정수해는 실시간에 적합한 MLAMBDA 기법과 비율테스트를 통한 정수해 검정기법을 통해 결정하였다.

• Journal of the Korean Society of Surveying, Geodesy, Photogrammetry and Cartography
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• v.14 no.2
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• pp.181-188
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• 1996

Geodetic Satellite Positioning Techniques (NNSS, Transit, Doppler, VLBI, SLR etc.) still have much difficulty in surveying and necessity of point positions is being amplified in korea. Therefore some research institutes have being investigated point positioning using the GPS. In this study, 1 arranged the theory deal with point positioning using GPS carrier beat phase of dual frequency and estimated corrections of errors that be included in GPS observable. Also, 1 determined point position by the differencing scheme of GPS carrier phase, and analyzed the accuracy of point position. 1 suggested potentiality of geodetic point positioning using GPS carrier phase by comparing result of relative positioning with result of point positioning and analyzing result of network adjustment fixed any point position.

• Bulletin of the Korean Space Science Society
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• 2005.10a
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• pp.68-68
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• 2005

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.8
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• pp.78-86
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• 2002

The GPS carrier phase measurements include integer ambiguities and the decorrelation process on the variance-covariance matrix is necessary to resolve these ambiguities efficiently. In this paper, we introduce a new method for the ambiguity de-correlation. This method divides the variance-covariance matrix into 4 smaller blocks and decorrelates them separately. The decorrelation of each block is processed recursively so that the result of the previous step is not affected by the next step. A couple of numerical examples chosen in random show that this method is better than or comparable to other decorrelation methods, however, the speed of this is relatively faster because the computations are performed on small blocks of the variance-covariance matrix.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.24 no.1
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• pp.10-15
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• 2016

In this study, The code-carrier divergence test was applied to GPS measurements, and the results were compared and analyzed. The GPS data used for the threshold determination were obtained from Global Navigation Satellite System permanent stations built by the Korea Aerospace Research Institute. At each permanent station, identical dual-frequency receiver and choke ring antenna with radome are installed. The analysis method, root mean square values were compared and analyzed for each permanent station and satellite. As a result, the root mean square value generally decreased as the satellite elevation angle increased although the trend was gentle. Threshold were finally selected based on the average and standard deviation of root mean square for each permanent station. For improving of availability and continuity in real-time operation when the threshold is over the limits, Code-Carrier divergence test values are initialized.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.12
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• pp.1032-1039
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• 2012

The present paper deals with precise relative positioning of formation satellites with long baseline in low Earth orbit making use of L1/L2 dual frequency GPS carrier phase measurements. Kinematic approach means to describe the motion of objects without taking its mass/dynamics model into consideration. The advantage of the kinematic approach is that information about dynamics of the system is not applied, which gives more flexibility and could improve the scientific interest of the observations made by the mission. The ionosphere terms, which are not canceled by double differenced measurement equation in the case of the long baseline, are explicitly estimated as unknown parameters by extended Kalman filter. The estimated float ambiguities by EKF are solved by existing efficient integer vector search strategy under integer least square condition. For the integer vector search, we employ well known MLAMBDA. Finally, The feasibility and accuracy of processing scheme are demonstrated using the GPS measurements for two satellites in low Earth orbit separated by baselines of 100 km.

• Bulletin of the Korean Space Science Society
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• 2001.04a
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• pp.34-34
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• 2001

• Journal of Advanced Navigation Technology
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• v.3 no.1
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• pp.13-19
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• 1999

Using GPS carrier phase whose cycle ambiguities are resolved, it is possible to perform precise survey requiring centimeter-level positioning accuracy. Because of an optical illusion, we cannot recognize the exact slope of Dokaebi Road. In this paper, we performed kinematic survey experiments in order to calculate the exact slope of Dokaebi Road with high positioning accuracy of CDGPS. By post-processing experimental data using CDGPS, it was possible to generate the exact vertical trajectory of Dokaebi Road with centimeter-level accuracy.