Performance analysis on carrier phase-based tightly-coupled GPS/BDS/INS integration in GNSS degraded and denied environments

Houzeng Han; Jian Wang; Jinling Wang; Xinglong Tan

doi:10.3390/s150408685

Performance analysis on carrier phase-based tightly-coupled GPS/BDS/INS integration in GNSS degraded and denied environments

Sensors (Basel). 2015 Apr 14;15(4):8685-711. doi: 10.3390/s150408685.

Authors

Houzeng Han¹, Jian Wang², Jinling Wang³, Xinglong Tan⁴

Affiliations

¹ School of Environment Science and Spatial Informatics, China University of Mining and Technology (CUMT), Xuzhou 221116, China. hanhouzeng@cumt.edu.cn.
² School of Environment Science and Spatial Informatics, China University of Mining and Technology (CUMT), Xuzhou 221116, China. wjian@cumt.edu.cn.
³ School of Civil and Environmental Engineering, University of New South Wales (UNSW), Sydney, NSW 2052, Australia. jinling.wang@unsw.edu.au.
⁴ School of Environment Science and Spatial Informatics, China University of Mining and Technology (CUMT), Xuzhou 221116, China. tanxinglong@cumt.edu.cn.

Abstract

The integration of Global Navigation Satellite Systems (GNSS) carrier phases with Inertial Navigation System (INS) measurements is essential to provide accurate and continuous position, velocity and attitude information, however it is necessary to fix ambiguities rapidly and reliably to obtain high accuracy navigation solutions. In this paper, we present the notion of combining the Global Positioning System (GPS), the BeiDou Navigation Satellite System (BDS) and low-cost micro-electro-mechanical sensors (MEMS) inertial systems for reliable navigation. An adaptive multipath factor-based tightly-coupled (TC) GPS/BDS/INS integration algorithm is presented and the overall performance of the integrated system is illustrated. A twenty seven states TC GPS/BDS/INS model is adopted with an extended Kalman filter (EKF), which is carried out by directly fusing ambiguity fixed double-difference (DD) carrier phase measurements with the INS predicted pseudoranges to estimate the error states. The INS-aided integer ambiguity resolution (AR) strategy is developed by using a dynamic model, a two-step estimation procedure is applied with adaptively estimated covariance matrix to further improve the AR performance. A field vehicular test was carried out to demonstrate the positioning performance of the combined system. The results show the TC GPS/BDS/INS system significantly improves the single-epoch AR reliability as compared to that of GPS/BDS-only or single satellite navigation system integrated strategy, especially for high cut-off elevations. The AR performance is also significantly improved for the combined system with adaptive covariance matrix in the presence of low elevation multipath related to the GNSS-only case. A total of fifteen simulated outage tests also show that the time to relock of the GPS/BDS signals is shortened, which improves the system availability. The results also indicate that TC integration system achieves a few centimeters accuracy in positioning based on the comparison analysis and covariance analysis, even in harsh environments (e.g., in urban canyons), thus we can see the advantage of positioning at high cut-off elevations that the combined GPS/BDS brings.