• Title/Summary/Keyword: 미지정수 결정

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Integer ambiguity propagation method for a precise positioning using GNSS carrier phase measurements (GNSS 반송파 위상을 이용한 정밀 측위에서 미지정수 전파기법)

  • Han, Deok-Hee;Yun, Hee-Hak;Park, Chan-Sik
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.37 no.7
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    • pp.678-684
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    • 2009
  • Many researches on the GNSS integer ambiguity resolution methods for precise positioning and attitude determination applications have been done. However, by the time invariant property of the integer ambiguity, the reuse of integer ambiguity without performing time consuming integer search procedure is possible. In this paper, a new efficient integer ambiguity propagation method is proposed. The initial integer ambiguity can be determined using the famous LAMBDA method and it is propagated with the propagation method. The proposed method can reconfigure the integer ambiguity using the previous epoch's integer ambiguity and new carrier phase measurements under environmental variations such as geometry changes, signal blockage and reacquisition. Experiments with real measurements show the proposed method can determine an integer ambiguity effectively.

실시간 다중 기준국 GNSS/GPS 반송파 미지정수 결정 기술 연구

  • Park, Jae-Ik;Lee, Eun-Seong;Heo, Mun-Beom
    • 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.

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Integer Ambiguity Resolution of L1 Carrier Phase Using LAMBDA Method (LAMBDA 방법에 의한 L1 반송파 미지정수 결정)

  • Kang, Joon-Mook;Park, Joung-Hyun;Sun, Jae-Hyun;Choi, Woong
    • Proceedings of the Korean Society of Surveying, Geodesy, Photogrammetry, and Cartography Conference
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    • 2003.04a
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    • pp.115-118
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    • 2003
  • 높은 정밀도를 갖는 상대위치결정은 매우 정밀한 반송파 측정값을 이용하며, 단기간에 높은 정밀도를 얻기 위해서는 미지정수가 결정되어야 한다. 본 논문에서는 LAMBDA 방법을 이용하여 이중차 미지정수를 해결하는 알고리즘을 정립하고, L1 반송파를 이용하여 상대위치를 결정하는 프로그램을 개발하였다.

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An Instantaneous Integer Ambiguity Resolution for GPS Real-Time Structure Monitoring (GPS 실시간 구조물 모니터링을 위한 반송파 관측데이터 순간미지정수 결정)

  • Lee, Hungkyu
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.34 no.1
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    • pp.341-353
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    • 2014
  • In order to deliver a centimeter-level kinematic positioning solution with GPS carrier-phase measurements, it is prerequisite to use correctly resolved integer ambiguities. Based on the mathematical modeling of GPS network with application of its geometrical constraints, this research has investigated an instantaneous ambiguity resolution procedure for the so-called 'integer constrained least-squares' technique which can be effectively implemented in real-time structure monitoring. In this process, algorithms of quality control for the float solutions and hypothesis tests using the constrained baseline for the ambiguity validation are included to enhance reliability of the solutions. The proposed procedure has been implemented by MATLAB, the language of technical computing, and processed field trial data obtained at a cable-stayed bridge to access its real-world applicability. The results are summarized in terms of ambiguity successful rates, impact of the stochastical models, and computation time to demonstrate performance of the instantaneous ambiguity resolution proposed.

GPS Carrier Multipath Estimation While Attitude Determination (자세결정시의 GPS 반송파 다중경로 오차 추정)

  • Lee, Eun-Sung;Chun, Se-Bum;Lee, Young-Jea;Kang, Tea-Sam;Jee, Gyu-In
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.3
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    • pp.65-70
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    • 2005
  • Incorrect ambiguity integer of GPS make a large error on attitude determination. In this paper one method is suggested for estimating the multipath of GPS carrier measurement while attitude determination. The multi-antenna system consists of 4 antennas have the same clock error help to make attitude determination effectively. If the distance between antennas is a half wavelength, it is not necessary to search the ambiguity integer and the multipath of GPS carrier measurement can be estimated. The results of the simulation are shown and analyzed.

Precise Relative Positioning for Formation Flying Satellite using GPS Carrier-phase Measurements (GPS 반송파 위상을 사용한 편대비행위성 상대위치결정 연구)

  • Park, Jae-Ik;Lee, Eunsung;Heo, Moon-Beom
    • 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.

A Comparative Analysis of Performance of Ambiguity Validation Methods (미지정수 후보 타당성 검정 기법간의 비교 분석)

  • Ko, Jae-Young;Shin, Mi-Young;Han, Young-Hoon;Cho, Deuk-Jae
    • Journal of Navigation and Port Research
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    • v.39 no.1
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    • pp.15-21
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    • 2015
  • In high precision positioning systems based on GNSS, ambiguity resolution is an important procedure. Correct ambiguity leads to positioning results which have high precision between millimeters and centimeters. However, when the ambiguity is determined incorrectly, ensuring accuracy and precision of the positioning result is impossible. An ambiguity validation test is required to obtain correct ambiguity when ambiguity resolution is performed based on the ILS (Integer Least Squares), which shows the best performance in point of theory and experiment when compared with other methods such as IR (Integer Rounding) and IB (Integer Bootstrapping). Comparison between the candidates of the validation test is needed to judge ambiguity correctly, because ILS searches for candidates of integer ambiguity, unlike other methods which calculate only one integer ambiguity. We analyzed the experimental performance of ambiguity validation tests. R-ratio, F-ratio and W-ratio were adopted for analysis. The performance of validation tests was evaluated by classifying normal operation, detection, missed detection and false alarm. As a result, strengths and weaknesses of validation tests was showed to experimental. we concluded that validation tests must be selected according to environment.

Improvement of Success Rate on LEO Satellite Attitude Determination Using GPS Carrier Phase Measurements (GPS를 이용한 저궤도 위성 자세 결정의 미지정수 결정 성공확률 향상)

  • Lee, Eun-Sung;Chun, Se-Bum;Lee, Young-Jea;Kang, Tea-Sam;Jee, Gyu-In;Jun, Hyang-Sig;Joo, Jung-Min
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.6
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    • pp.45-50
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    • 2005
  • To determine precise position GPS carrier phase measurements are used. In addition, the multi-antenna system consisting of 2 or more GPS antennas can make attitude determination effectively. When GPS carrier phase measurements are used the integer ambiguity must be fixed. The success rate is used to validate the integer ambiguity. For LEO satellite attitude determination the double difference carrier phase measurements are used, the success rate is calculated using the covariance matrix and the measurement matrix. The constraint that LEO satellite position vector and attitude vector is orthogonal is suggested for improving the success rate. The LEO satellite orbit model is KITSAT3. The results of the simulation are shown and analyzed.

Ambiguity Determination Technique for Multiple GPS Reference Stations using the Combination of L1/L2 Carrier Phase (L1/L2 측정치 조합을 이용한 GPS 기준국간 반송파 미지정수 결정 기법)

  • Park, Byung-Woon;Song, June-Sol;Kee, Chang-Don
    • Journal of Advanced Navigation Technology
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    • v.15 no.5
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    • pp.705-713
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    • 2011
  • In this paper, we introduce two techniques for resolving integer ambiguities between reference stations, which is one of the most important processes in Network RTK correction generation process. Each techniques uses Hatch filter and combination of L1/L2 measurements and we used simulation data and real data to evaluate performance of the techniques. For evaluating performance of each technique, we compared corrections generated from user site and Network RTK. As a result, Network RTK with the technique which uses Hatch filter improves user performance much more than single baseline RTK does. Residual of user is smaller than a half size of wavelength so it does not affect user integer ambiguity resolution, however, it contains significant bias error. On the other hand, when we used the technique which uses combination of L1/L2 measurements, residual error of user is largely reduced compared to the technique using Hatch filter.

Precise Positioning using GPS and Pseudolite (의사위성과 GPS틀 이용한 정밀 위치 결정)

  • Yun, Hee-Hak;Kang, Dong-Youn;Shin, Mi-Young;Park, Chan-Sik;Lee, Sang-Jeong
    • Proceedings of the KIEE Conference
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    • 2007.10a
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    • pp.95-96
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    • 2007
  • GPS를 사용할 경우 반송파 위상 측정치를 이용한 정밀한 위치 측정이 가능하다. 그러나 GPS만을 사용할 경우, 미지정수 결정 성공률이 낮으며, 도심과 같은 곳에서 신호를 수신하지 못하는 경우가 발생한다. 이 문제는 의사위성을 추가하여 해결할 수 있다. 본 논문에서는 GPS에 의사위성을 추가하여 미지정수의 결정 성공률이 향상되고 가용성을 향상시킬 수 있으며 정확도가 향상됨을 보였다.

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