Developed with Research Team of Prof Shunsuke Kamijo from University of Tokyo.
We develop a rectified positioning method using a basic 3-dimension city building model and ray-tracing simulation to mitigate the signal reflection effects. This proposed method is achieved by implementing a particle filter to distribute possible position candidates. The likelihood of each candidate is evaluated based on the similarity between the pseudorange measurement and simulated pseudorange of the candidate. Finally, the expectation of all the candidates is the rectified positioning of the proposed map method. The real data are recorded at an urban canyon environment in the Chiyoda district of Tokyo using a commercial grade u-blox GNSS receiver. Both static and dynamic tests were performed. With the aid of GLONASS and QZSS, it is shown that the proposed method can achieve a 4.4 meters 1σ positioning error in the tested urban canyon area.
Demonstration of distribution of particles and final estimated position using the 3DMA GNSS Positioning method.
Calculation of the pseudorange similarity using the measured pseudorange from GNSS receiver and simulated pseudorange by 3D building and ray-tracing.
This study first develops an algorithm to detect NLOS signals from the pseudorange measurements by using a 3D building model, ray-tracing simulation, and known receiver position.
According to the analysis of 24 hours of collected NLOS data, a new finding is that NLOS pseudorange delay is highly correlated with the elevation angle of satellite instead of the received signal strength.
Thus, we further propose an innovative NLOS model using two variables, the elevation angle and the distance between the receiver and building that reflect the NLOS. The proposed model is evaluated in both pseudorange and position domains. Based on the experiment results regarding pseudorange error, the difference between the proposed model and the collected NLOS measurement is very small.
Skyplots with surrounding building information of data collected in Kowloon. the color of satellite trajectory denotes C/N0, the redder the color the higher is the C/N0 received.
NLOS pseudorange error with respect to elevation angle of the 24-hours data. The color denotes the carrier to noise ratio of each point.
Illustration of a reflecting signal that followed the law of reflection.
Mean and standard deviation of all the NLOS delays reflected at same wall from different SVs.