Abstract:For improved positioning in urban canyons, this study proposes an efficient dual‐filter method integrating multi‐constellation global navigation satellite system (GNSS), an inertial navigation system (INS), a barometric altimeter and an on‐board diagnostics (OBD) module. The proposed method consists of a position‐domain (PD) Hatch filter and velocity Kalman filter. The Hatch filter is operated as the main positioning filter and the Kalman filter is operated as a sub‐filter to aid the main filter for the occasi… Show more
“…When utilising the carrier phase measurements, cycle slips and multipath errors need to be detected carefully. For this purpose, the Fault Detection Exclusion (FDE) algorithm [6,32] is applied. In this manner, the proposed CSCKF-based VIG system provides globally consistent and robust pose estimates even in the GNSSdegraded environments.…”
“…In order to overcome the time‐increasing INS errors, the integration of the Global Navigation Satellite System (GNSS) and INS has been an effective alternative [4, 5]. By utilising GNSS receivers, the integrated system is not confined by estimating local [6] DoF poses but it can also provide globally referenced position estimates. In recent years, the development of multi‐GNSS boosted the progress of INS/GNSS systems.…”
Section: Introductionmentioning
confidence: 99%
“…[7] demonstrated that a multi‐GNSS system provides better performance than a Global Positioning System (GPS)‐only system for INS augmentation. However, the performance of GNSS is strongly influenced by abnormal signal conditions occurred in urban canyons and tunnels [6]. For instance, if the time length of GNSS signal outages is long, the positioning accuracy provided by any INS/GNSS system will be degraded due to the rapid accumulation of INS errors.…”
Efficient multi‐sensor fusion is crucial to provide accurate pose estimates for navigating various next‐generation autonomous vehicles such as self‐driving cars, personal air vehicles, urban air mobilities, and electronic vertical take‐off and landing aircraft with respect to a unified global reference frame. The integration of the Global Navigation Satellite System (GNSS) and Inertial Navigation System (INS) provides globally uniform coordinate information, and the Visual‐Inertial Odometry (VIO) gives stable and accurate local pose estimates. However, the error of the integrated INS/GNSS increases rapidly in GNSS‐challenged environments, and the VIO system suffers from the long‐term error accumulation. To cope with these difficulties, this paper proposes a new tightly coupled Visual‐Inertial‐GNSS (VIG) system to achieve robust and drift‐free pose estimation utilising GNSS raw measurements, image features, and inertial measurements. A novel compressed state constraint Kalman Filter (CSCKF) is formulated to combine time‐propagated feature measurements and differential GNSS observations to aid INS. Compared to the conventional integrated navigation systems, the proposed CSCKF‐based VIG system is advantageous in maintaining the minimum number of states without unnecessary state augmentation and no loss of performance. The proposed system is evaluated by field experiments in different GNSS availability situations. The results show that accuracy is improved significantly in GNSS‐degraded environments compared to that of the conventional systems.
“…When utilising the carrier phase measurements, cycle slips and multipath errors need to be detected carefully. For this purpose, the Fault Detection Exclusion (FDE) algorithm [6,32] is applied. In this manner, the proposed CSCKF-based VIG system provides globally consistent and robust pose estimates even in the GNSSdegraded environments.…”
“…In order to overcome the time‐increasing INS errors, the integration of the Global Navigation Satellite System (GNSS) and INS has been an effective alternative [4, 5]. By utilising GNSS receivers, the integrated system is not confined by estimating local [6] DoF poses but it can also provide globally referenced position estimates. In recent years, the development of multi‐GNSS boosted the progress of INS/GNSS systems.…”
Section: Introductionmentioning
confidence: 99%
“…[7] demonstrated that a multi‐GNSS system provides better performance than a Global Positioning System (GPS)‐only system for INS augmentation. However, the performance of GNSS is strongly influenced by abnormal signal conditions occurred in urban canyons and tunnels [6]. For instance, if the time length of GNSS signal outages is long, the positioning accuracy provided by any INS/GNSS system will be degraded due to the rapid accumulation of INS errors.…”
Efficient multi‐sensor fusion is crucial to provide accurate pose estimates for navigating various next‐generation autonomous vehicles such as self‐driving cars, personal air vehicles, urban air mobilities, and electronic vertical take‐off and landing aircraft with respect to a unified global reference frame. The integration of the Global Navigation Satellite System (GNSS) and Inertial Navigation System (INS) provides globally uniform coordinate information, and the Visual‐Inertial Odometry (VIO) gives stable and accurate local pose estimates. However, the error of the integrated INS/GNSS increases rapidly in GNSS‐challenged environments, and the VIO system suffers from the long‐term error accumulation. To cope with these difficulties, this paper proposes a new tightly coupled Visual‐Inertial‐GNSS (VIG) system to achieve robust and drift‐free pose estimation utilising GNSS raw measurements, image features, and inertial measurements. A novel compressed state constraint Kalman Filter (CSCKF) is formulated to combine time‐propagated feature measurements and differential GNSS observations to aid INS. Compared to the conventional integrated navigation systems, the proposed CSCKF‐based VIG system is advantageous in maintaining the minimum number of states without unnecessary state augmentation and no loss of performance. The proposed system is evaluated by field experiments in different GNSS availability situations. The results show that accuracy is improved significantly in GNSS‐degraded environments compared to that of the conventional systems.
“…However, satellite signals are frequently blocked or even lose lock in complex urban scenarios, which cannot guarantee the effectiveness of positioning [ 3 ]. Inertial Navigation System (INS) has the advantages of strong autonomy and strong anti-interference and can obtain short-term, high-precision navigation and positioning results [ 4 ]. However, INS errors accumulate over time, and long-term independent solution can result in reduced accuracy or even divergence [ 5 ].…”
Due to the massive multipath effects and non-line-of-sight (NLOS) signal receptions, the accuracy and reliability of GNSS positioning solution can be severely degraded in a highly urbanized area, which has a negative impact on the performance of GNSS/INS integrated navigation. Therefore, this paper proposes a multipath/NLOS detection method based on the K-means clustering algorithm for vehicle GNSS/INS integrated positioning. It comprehensively considers different feature parameters derived from GNSS raw observations, such as the satellite-elevation angle, carrier-to-noise ratio, pseudorange residual, and pseudorange rate consistency to effectively classify GNSS signals. In view of the influence of different GNSS signals on positioning results, the K-means clustering algorithm is exploited to divide the observation data into two main categories: direct signals and indirect signals (including multipath and NLOS signals). Then, the multipath/NLOS signal is separated from the observation data. Finally, this paper uses the measured vehicle GNSS/INS observation data, including offline dataset and online dataset, to verify the accuracy of signal classification based on double-differenced pseudorange positioning. A series of experiments conducted in typical urban scenarios demonstrate that the proposed method could ameliorate the positioning accuracy significantly compared with the conventional GNSS/INS integrated navigation. After excluding GNSS outliers, the positioning accuracy of the offline dataset is improved by 16% and 85% in the horizontal and vertical directions, respectively, and the positioning accuracy of the online dataset is improved by 21% and 41% in the two directions. This method does not rely on external geographic information data and other sensors, which has better practicability and environmental adaptability.
“…In the range domain, it is a trend to reform the CSC parameters for a better position solution, such as smoothing window width [7,8], alternative observation selection [9] and ionosphere mathematical method [10], which sometimes may lead to position divergence [11]. In the position domain, phase-connected filter, Hatch filter with Kalmantype gain and covariance estimation method are proposed [12][13][14] to cope with the structure shortage in the CSC smoothing process, which can solve the weakness of the range-domain method well, but always require strict parameter estimation. Besides, due to external correction data, the CSC method performs well and is widely used in augmentation systems since many error sources ignored by the CSC method, especially the ionospheric delay, can be eliminated.…”
Currently, single-frequency Global Navigation Satellite System (GNSS) receivers dominate maritime navigation units due to their simple structure and low cost but usually cannot meet the positioning requirements of Maritime Autonomous Surface Ship (MASS). Herein, a novel adaptive Doppler-smoothed-code Bilateral Kernel Regression (DBKR) method is proposed, which improves pseudorange accuracy in the range domain and then reconstructs observations in the position domain. In the range domain, the Doppler observable is utilised to smooth the pseudorange with an optimal window smoothing width for the BeiDou Navigation Satellite System (BDS) receiver to alleviate ionosphere delay. In the position domain, we elaborate a bilateral kernel regression model to further reduce the positioning drift. The on-line regression process starts with mapping the observation space to Euclidean space and subsequently fusing all observations of the same epoch using the Gaussian Radial Basis Function (RBF). Finally, the experiments under static and dynamic scenarios are carried out, which verify the validity and efficiency of the proposed DBKR method.
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