4.2 DoA/RSS Estimation Using Sectorized Antennas
4.2.4 Numerical Evaluation and Comparison
In the evaluation of the estimators and CRBs discussed in the previous sections, we
will be considering two different antenna models. On the one hand, we assume an ESA
with M = 6 sectors and, on the other hand, we use the LWA model from [P2]. This
model was obtained by approximating the measured radiation patterns of the LWA [81]
according to the procedure described later in Section 4.4. The resulting model consists
of M = 12 sectors each approximated by a Gaussian radiation pattern (4.1) with the
parameters listed in [P2, Tab. III]. The ESA can be used in combination with any of
the discussed estimators, whereas the LWA consists of sectors where the main beam is
different in all sectors meaning that it can be used with TSLS only (see [P2]). For the
ESA, we use TSLS with L = 3 and variance weighting, which results in the overall best
performance [P2]. The influence of L and the weighting scheme on the performance of
TSLS is then studied using the LWA.
All results presented in the following were obtained assuming a DoA uniformly
distributed over the whole angular coverage area of the respective antennas. This
means that the DoA is distributed as Ï
k≥ U(≠180
¶; 180
¶) for the ESA and as Ï
k≥
U(≠60
¶; 60
¶) for the LWA. An overview of the expressions used in the figures can be
found in Tables 4.2 and 4.3. For a detailed description of the simulation setup please
refer to the references in those tables.
Figures 4.6 and 4.7 depict the performance of DoA estimation and RSS estimation
with the ESA as a function of the SSP a
s, respectively. We notice that, in certain
conditions, both SLS and TSLS result in an RMSE that is lower than the respective
4.2 DoA/RSS Estimation Using Sectorized Antennas Tab. 4.3. Expressions used in the evaluation of RSS estimation performance.
Expression Alg./CRB Type References
RRMSERSS CRB numerical average over DoA (4.19), [P1]
RRMSEa
RSS CRB approximation, numerical average over DoA (4.21), [P1]
RRMSESNRRSS CRB asymptotical SNR æ Œ, analytical (4.25), [P1]
RRMSEN
RSS,m MaxE asymptotical N æ Œ, analytical (4.45), [P4]
SLS SLS numerical algorithm evaluation Sec. 4.2.2.2, [P5]
Side-sector suppression, as 0 0.2 0.4 0.6 0.8 1 RM S E ˆϕ [d eg] 10-1 100 101 102 103 RMSEDoA RMSEaDoA RMSESNRDoA SLS RMSESLS RMSENDoA,m TSLS
Fig. 4.6. DoA estimation performance as a function of the side-sector suppression. Parameters: ESA
with M = 6, N = 100, and SNR = 5 dB.
CRB. Clearly, this indicates that both algorithms are not entirely unbiased. As shown
and discussed in [P2] and [P5], a significant non-zero bias in SLS and TSLS occurs in
adverse operation conditions, such as for a low SNR, for strong multipath or for antennas
with disadvantageous values for the SSP. Now the choice of the SSP is a compromise.
As can be seen from the asymptotic CRB in Figure 4.6, the SSP should be as small
as possible for SNR æ Œ. However, for moderate to large SNR, the lowest CRB is
attained for a SSP around a
sœ [0.2; 0.4]. This is in line with the SSP interval where the
DoA estimators SLS and TSLS result in the lowest RMSE. However, as evident from
Figure 4.6 TSLS is much less susceptible to the choice of a
sthan SLS. For RSS estimation
and SNR æ Œ, the asymptotic CRB is entirely independent of a
s. However, for finite
SNR, the trend in the RSS estimation CRB is opposite to the trend in RMSE
SNRDoAas an
omnidirectional antenna (a
s= 1) results in the lowest CRB. Overall, a SSP a
sœ [0.2; 0.4]
is thus a good compromise. Consequently, the approximations RMSE
aDoAand RMSE
aRSSare very accurate for well-tuned antennas since the respective curves in Figures 4.6 and
4.7 match perfectly with the CRBs for a
s>0.1.
Figures 4.6 and 4.7 also include the asymptotic RMSEs N æ Œ of MaxE DoA and
RSS estimation. Even in the asymptotic case, the performance of MaxE is far from the
Side-sector suppression, as 0 0.2 0.4 0.6 0.8 1 RRM S E ˆγ 10-3 10-2 10-1 100 101 RRMSERSS RRMSEaRSS RRMSESNRRSS SLS RRMSENRSS,m
Fig. 4.7. RSS estimation performance as a function of the side-sector suppression. Parameters: ESA
with M = 6, N = 100, and SNR = 5 dB.
CRBs and the performance of SLS and TSLS with finite N. Note that for the asymptotic
case N æ Œ, the other estimators as well as the CRB result in an RMSE = 0. Due to
this significant difference in performance, we will, in the following, not discuss MaxE
anymore. For a detailed performance discussion of MaxE refer to [P4] and [P5] instead.
Figure 4.8 depicts the performance of DoA estimation with an ESA as a function of
the SNR. As can be seen, RMSE
aDoA
is a perfect approximation for the CRB RMSE
DoAand the analytical expression for the RMSE of SLS is also very accurate for SNR > 2 dB.
Moreover, for moderate SNRs around 5 dB both SLS and TSLS perform quite close to
the CRB. For increasing SNRs, TSLS approaches the CRB even closer. The performance
of SLS, in contrast, saturates at a much higher level (RMSE
SNRSLS) than the CRB for
SNR > 15 dB. As discussed in more detail in [P1], this is due to SLS excluding all but
two sectors from the DoA estimation. For increasing SNRs, our assumption that all
but two sectors are too noisy to exploit the TN signal component becomes increasingly
worse. For low SNRs, on the other hand, the performance of TSLS and SLS is in fact
equal. This is due to the weighting in TSLS, which practically excludes all other but
the two sectors that are also used in SLS.
In TSLS the number of sectors L that results in the best performance depends on
the type of antenna, as well as on the SNR. This is illustrated in Figure 4.9 using the
LWA as an example. For large SNRs, the best performance is achieved with L = 11,
i.e., with significantly more sectors compared to the ESA. While the ESA has M = 6
sectors with a beam-width — ¥ 0.22 rad distributed over 360°, the LWA has M = 12
sectors with beam-widths between 0.5 rad and 0.7 rad distributed over 120° [P1]. This
means that the number of sectors that receive the TN signal with a significant signal
strength is much larger in the LWA than in the ESA. Consequently, L should also be
4.3 Localization Using Sectorized Antennas