• 제목/요약/키워드: combined navigation

검색결과 257건 처리시간 0.026초

Evaluation of Navigation System Performance of GPS/GLONASS/Galileo/BeiDou/QZSS System using High Performance GNSS Receiver

  • Park, Yong-Hui;Jeong, Jin-Ho;Park, Jin-Mo;Park, Sung-Hyun
    • Journal of Positioning, Navigation, and Timing
    • /
    • 제11권4호
    • /
    • pp.333-339
    • /
    • 2022
  • The satellite navigation system was developed for the purpose of calculating the location of local users, starting with the Global Positioning System (GPS) in the 1980s. Advanced countries in the space industry are operating Global Navigation Satellite System (GNSS) that covers the entire earth, such as GPS, GLONASS, Galileo, and BeiDou, by establishing satellite navigation systems for each country. Regional Navigation Satellite Systems (RNSS) such as QZSS and NavIC are also in operation. In the early 2010s, only GPS and GLONASS could calculate location using a single system for location determination. After 2016, the EU and China also completed the establishment of GNSS such as Galileo and BeiDou. As a result, satellite navigation users can benefit from improved availability of GNSS. In addition, before Galileo and BeiDou's Full Operational Capability (FOC) declaration, they used combined navigation algorithms to calculate the user's location by adding another satellite navigation system to the GPS satellites. Recently, it may be possible to calculate a user's location for each navigation system using the resources of a single system. In this paper, we evaluated the performance of single system navigation and combined navigation solutions of GPS, GLONASS, Galileo, BeiDou and QZSS individual navigation systems using high-performance GNSS receivers.

Characteristics of Relative Navigation Algorithms Using Laser Measurements and Laser-GPS Combined Measurements

  • Kang, Dae-Eun;Park, Sang-Young;Son, Jihae
    • Journal of Astronomy and Space Sciences
    • /
    • 제35권4호
    • /
    • pp.287-293
    • /
    • 2018
  • This paper presents a satellite relative navigation strategy for formation flying, which chooses an appropriate navigation algorithm according to the operating environment. Not only global positioning system (GPS) measurements, but laser measurements can also be utilized to determine the relative positions of satellites. Laser data is used solely or together with GPS measurements. Numerical simulations were conducted to compare the relative navigation algorithm using only laser data and laser data combined with GPS data. If an accurate direction of laser pointing is estimated, the relative position of satellites can be determined using only laser measurements. If not, the combined algorithm has better performance, and is irrelevant to the precision of the relative angle data between two satellites in spherical coordinates. Within 10 km relative distance between satellites, relative navigation using double difference GPS data makes more precise relative position estimation results. If the simulation results are applied to the relative navigation strategy, the proper algorithm can be chosen, and the relative position of satellites can be estimated precisely in changing mission environments.

Analysis of the Combined Positioning Accuracy using GPS and GLONASS Navigation Satellites

  • Choi, Byung-Kyu;Roh, Kyoung-Min;Lee, Sang Jeong
    • Journal of Positioning, Navigation, and Timing
    • /
    • 제2권2호
    • /
    • pp.131-137
    • /
    • 2013
  • In this study, positioning results that combined the code observation information of GPS and GLONASS navigation satellites were analyzed. Especially, the distribution of GLONASS satellites observed in Korea and the combined GPS/GLONASS positioning results were presented. The GNSS data received at two reference stations (GRAS in Europe and KOHG in Goheung, Korea) during a day were processed, and the mean value and root mean square (RMS) value of the position error were calculated. The analysis results indicated that the combined GPS/GLONASS positioning did not show significantly improved performance compared to the GPS-only positioning. This could be due to the inter-system hardware bias for GPS/GLONASS receivers, the selection of transformation parameters between reference coordinate systems, the selection of a confidence level for error analysis, or the number of visible satellites at a specific time.

Combined GPS/BeiDou Positioning Performance in South Korea

  • Choi, Byung-Kyu;Cho, Chang-Hyun;Lee, Sang Jeong
    • Journal of Positioning, Navigation, and Timing
    • /
    • 제3권4호
    • /
    • pp.149-154
    • /
    • 2014
  • The BeiDou is a satellite-based positioning and navigation system, which is under construction by the China Satellite Navigation Office. Until the June of 2014, the constellation of BeiDou navigation satellite system consists of 14 satellites including five geostationary earth orbit (GEO), five inclined geosynchronous earth orbit (IGSO) and four medium earth orbit (MEO). In this paper, we present the positioning results using BeiDou B1 code measurements obtained from three GNSS reference stations (BHAO, SKMA, MKPO). Combined Beidou/GPS positioning results are also compared to BeiDou and GPS only. BeiDou-only positioning errors for the east-west and north-south direction had less than 2 meter with root mean square (RMS) value. However, the positioning error for the up-down direction had larger than 10 meter at a 95% confidence level. Our results also suggest that the position precision is improved by combined BeiDou/GPS compared to BeiDou-only.

Design of Trajectory Generator for Performance Evaluation of Navigation Systems

  • Jae Hoon Son;Sang Heon Oh;Dong-Hwan Hwang
    • Journal of Positioning, Navigation, and Timing
    • /
    • 제12권4호
    • /
    • pp.409-421
    • /
    • 2023
  • In order to develop navigation systems, simulators that provide navigation sensors data are required. A trajectory generator that simulates vehicle motion is needed to generate navigation sensors data in the simulator. In this paper, a trajectory generator for evaluating navigation system performance is proposed. The proposed trajectory generator consists of two parts. The first part obtains parameters from the motion scenario file whereas the second part generates position, velocity, and attitude from the parameters. In the proposed trajectory generator six degrees of freedom, halt, climb, turn, accel turn, spiral, combined, and waypoint motions are given as basic motions with parameters. These motions can be combined to generate complex trajectories of the vehicle. Maximum acceleration and jerk for linear motion and maximum angular acceleration and velocity for rotational motion are considered to generate trajectories. In order to show the usefulness of the proposed trajectory generator, trajectories were generated from motion scenario files and the results were observed. The results show that the proposed trajectory generator can accurately simulate complex vehicle motions that can be used to evaluate navigation system performance.

Development of a Combined GPS/GLONASS PPP Method

  • Choi, Byung-Kyu;Roh, Kyoung-Min;Lee, Sang Jeong
    • Journal of Positioning, Navigation, and Timing
    • /
    • 제3권1호
    • /
    • pp.31-36
    • /
    • 2014
  • Precise Point Positioning (PPP) is a stand-alone precise positioning approach. As the quality of satellite orbit and clock products from analysis centers has been improved, PPP can provide more precise positioning accuracy and reliability. A combined use of Global Positioning System (GPS) and Global Orbiting Navigation Satellite System (GLONASS) in PPP is now available. In this paper, we explained about an approach for combined GPS and GLONASS PPP measurement processing, and validated the performance through the comparison with GPS-only PPP results. We also used the measurement obtained from the GRAS reference station for the performance validation. As a result, we found that the combined GPS/GLONASS PPP can yield a more precise positioning than the GPS-only PPP.

GPS/GLONASS의 반송파 위상을 이용한 차량항법 (Vehicle Navigation using Carrier Phase of GPS/GLONASS)

  • 이인수;이용희;문두열;손영동
    • 한국항해항만학회지
    • /
    • 제26권3호
    • /
    • pp.303-310
    • /
    • 2002
  • 현재 범세계위치결정체계(GPS)와 추측항법(DR), 기타 장치를 결합한 육상차량항법시스템이 사용되고 있다. 그리고 GPS는 육상항법시스템으로 널리 이용되고 있지만, 도심지 등에서 가시위성의 부족으로 차량의 동적 위치결정에 적절하지 못하다. 따라서 본 연구에서는 GPS의 단점을 보완하기 위해 GPS/GLONASS 결합항법시스템을 이용하여 차량의 동적위치를 결정하였다. 실험결과 도심지에서 많은 장애물과 가시위성에도 불구하고 GLONASS 위성의 부가로 높은 자료획득률을 보여 GPS/GLONASS의 결합항법시스템으로 차량의 동적 위치를 연속적으로 획득할 수 있었다. 그러므로 GPS/GLONASS 결합항법시스템은 도로의 교통흐름의 통제와 효율적 관리에 응용할 수 있을 것으로 사료된다.

Combined GPS/GLONASS Relative Receiver DCB Estimation Using the LSQ Method and Ionospheric TEC Changes over South Korea

  • Choi, Byung-Kyu;Yoon, Ha Su;Lee, Sang Jeong
    • Journal of Positioning, Navigation, and Timing
    • /
    • 제7권3호
    • /
    • pp.175-181
    • /
    • 2018
  • The use of dual-frequency measurements from the Global Navigation Satellite System (GNSS) enables us to observe precise ionospheric total electron content (TEC). Currently, many GNSS reference stations in South Korea provide both GPS and GLONASS data. In the present study, we estimated the grid-based TEC values and relative receiver differential code biases (DCB) from a GNSS network operated by the Korea Astronomy and Space Science Institute. In addition, we compared the diurnal variations in a TEC time series from solutions of the GPS only, the GLONASS only, and combined GPS/GLONASS processing. A significant difference between the GPS only TEC and combined GPS/GLONASS TEC at a specific grid point over South Korea appeared near the solar terminator. It is noted that GLONASS measurements can contribute to observing a variation in ionospheric TEC over high latitude regions.

Improved GPS-based Satellite Relative Navigation Using Femtosecond Laser Relative Distance Measurements

  • Oh, Hyungjik;Park, Han-Earl;Lee, Kwangwon;Park, Sang-Young;Park, Chandeok
    • Journal of Astronomy and Space Sciences
    • /
    • 제33권1호
    • /
    • pp.45-54
    • /
    • 2016
  • This study developed an approach for improving Carrier-phase Differential Global Positioning System (CDGPS) based realtime satellite relative navigation by applying laser baseline measurement data. The robustness against the space operational environment was considered, and a Synthetic Wavelength Interferometer (SWI) algorithm based on a femtosecond laser measurement model was developed. The phase differences between two laser wavelengths were combined to measure precise distance. Generated laser data were used to improve estimation accuracy for the float ambiguity of CDGPS data. Relative navigation simulations in real-time were performed using the extended Kalman filter algorithm. The GPS and laser-combined relative navigation accuracy was compared with GPS-only relative navigation solutions to determine the impact of laser data on relative navigation. In numerical simulations, the success rate of integer ambiguity resolution increased when laser data was added to GPS data. The relative navigational errors also improved five-fold and two-fold, relative to the GPS-only error, for 250 m and 5 km initial relative distances, respectively. The methodology developed in this study is suitable for application to future satellite formation-flying missions.

GPS/ GLONASS 통합 수신용 RF 전단부의 설계 및 제작 (Design and Implementation of Combined RF Receiver Front End for GPS/GLONASS)

  • 주재순;염경환;이상정
    • 한국전자파학회논문지
    • /
    • 제12권4호
    • /
    • pp.494-502
    • /
    • 2001
  • GPS(Global Positiong System)와 GLONASS(GLObal NAvigation Satellite System) 는 위치와 시각을 제공하는 기초 기술이며 항법 분야, 측지분야, 자세 측정 및 제어 분야 등 그 응용분야가 다양하다. 그러나 GPS나 GLONASS는 각기 제한된 가시 위성의 수로 인해 정확한 항법 해를 얻는데 어려움이 있으며, 또한 하나의 항법 시스템만을 이용하는 경우 의존도가 너무 높아지게 되어 전략적인 측면에서도 불리하다. 이러한 측면에서 GPS와 GLONASS 의 통합수신은 보다 정확한 항법 해를 구할 수 있고 보다 나은 시스템의 안정도를 가져올 수 있다. 이를 목적으로 GPS/GLONSS 통합 수신용 RF 전단부를 130$\times$80 mm$^2$의 PCB상에 구현하였고 실제 시스템에 적용 가능한지를 측정하였으며 GLONASS 수신기의 one chip화의 가능성을 검토하였다.

  • PDF