alt="Photos depict LTE environment layout and experimental hardware setup."/>
Figure 38.49 LTE environment layout and experimental hardware setup. Map data: Google Earth (Shamaei et al. [63]).
Source: Reproduced with permission of Z. Kassas (International Technical Meeting Conference).
Figure 38.50 (a) Estimated change in pseudorange and estimated CIR at t = 13.04 s for eNodeB 1. The change in the pseudorange was calculated using (1) SSS pseudoranges, (2) SSS+CRS pseudoranges, and (3) true ranges obtained using GPS. (b) Pseudorange error between (1) GPS and SSS and (2) GPS and SSS+CRS. (c) CDF of the error in (b) (Shamaei et al. [63]).
Source: Reproduced with permission of Z. Kassas (International Technical Meeting Conference).
Figure 38.51 (a) Estimated change in pseudorange and estimated CIR at t = 8.89 s and t = 40.5 s for eNodeB 2. The change in the pseudorange was calculated using (1) SSS pseudoranges, (2) CRS pseudoranges, and (3) true ranges obtained using GPS. (b) Pseudorange error between (1) GPS and SSS and (2) GPS and SSS+CRS. (c) CDF of the error in (b) (Shamaei et al. [63]).
Source: Reproduced with permission of Z. Kassas (International Technical Meeting Conference).
The error in the pseudorange obtained by tracking the SSS is mainly due to multipath. The estimated CIR at t = 13.04 s for eNodeB 1 and t = 8.89 s and t = 40.5 s for eNodeB 2 show several peaks due to multipath, which are dominating the line‐of‐sight (LoS) peak. These peaks contributed a pseudorange error of around 330 m at t = 13.04 s for eNodeB 1 and around 130 m at t = 8.89 s for eNodeB 2. These results highlight the importance of utilizing the CRS signals to correct for multipath‐induced errors.
38.6.4.2 Ground Vehicle Navigation
A car was equipped with the cellular LTE navigation receiver discussed in Section 38.6.2. The receiver was tuned to the cellular carrier frequencies 739 MHz and 1955 MHz, which are used by the US cellular provider AT&T. The PLL, FLL, and DLL noise‐equivalent bandwidths were set to 4, 0.2, and 0.001 Hz, respectively. The adaptive threshold approach proposed in [65] was adopted to mitigate multipath.
All measurements and trajectories were projected onto a 2D plane. It was assumed that the receiver had access to GPS, and GPS was cut off at the start time of the experiment. Therefore, the EKF’s states were initialized with the values obtained from the GPS navigation solution. The standard deviation of the initial uncertainty of position and velocity were set to be 5 m and 0.01 m/s, respectively [55]. The standard deviation of the initial uncertainty of the clock bias and drift were set to be 0.1 m and 0.01 m/s, which were obtained empirically. The clock oscillators were modeled as oven‐controlled crystal oscillators (OCXOs) with
38.6.4.3 Aerial Vehicle Navigation
A UAV was equipped with the cellular LTE navigation receiver discussed in Section 38.6.2. When a UAV flies high enough, the received signal to the UAV does not experience multipath from the surrounding environment, except from the UAV’s body. Here, the multipath effect from the UAV’s body is negligible; therefore, tracking only the SSS yields good results, and the CRS was not used. This significantly decreases the computational burden in the receiver. It also reduces the need for a high sampling rate, which lowers the hardware cost and size. The receiver was tuned to the cellular carrier frequency of 1955 MHz, which is used by the US cellular provider AT&T.
Over the course of the experiment, the UAV was flying at an altitude of 40 m. The receiver was listening to three eNodeBs, each of which had two transmitting antennas with 20 MHz transmission bandwidth. The positions of the eNodeBs were mapped prior to the experiment with approximately 2 m accuracy. All measurements and trajectories were projected onto a 2D plane. Subsequently, only the horizontal position of the receiver was estimated. It was assumed that the receiver had access to GPS, and GPS was cut off at the start time of the experiment. Therefore, the EKF’s states were initialized with the values obtained from the GPS navigation solution. The EKF process noise and measurement noise covariances were set in a similar manner to the ground vehicle navigation experiment. The environment layout as well as the true and estimated receiver trajectories are shown in Figure 38.53. It can be seen from Figure 38.53 that the navigation solution obtained from LTE signals closely follows the GPS navigation solution. The ground‐truth trajectory was obtained from the GRID GPS SDR [58].
In an urban environment, the pseudoranges received by a ground vehicle will suffer from more multipath‐induced error compared to the pseudoranges received by a UAV with LoS conditions. However, this comparison can be made as long as the ground vehicle and UAV are navigating in the same environment, using the same eNodeBs, and following the same trajectories, except that one is on the ground while the other is airborne. In the results presented in Figures 38.52 and 38.53, the ground vehicle was equipped with a better USRP than the one on the UAV, due to payload limitations. Consequently, the LTE receiver onboard the ground vehicle was able to listen to more eNodeBs than the receiver onboard the UAV, providing the
