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Article

Making Automotive Radar Sensor Validation Measurements Comparable

Institute of Automotive Engineering, Technical University of Darmstadt, Otto-Berndt-Straße 2, 64287 Darmstadt, Germany
*
Author to whom correspondence should be addressed.
Appl. Sci. 2023, 13(20), 11405; https://doi.org/10.3390/app132011405
Submission received: 28 August 2023 / Revised: 6 October 2023 / Accepted: 14 October 2023 / Published: 17 October 2023

Abstract

:
Virtual validation of radar sensor models is becoming increasingly important for the safety validation of Light Detection and Rangings (lidars). Therefore, methods for quantitative comparison of radar measurements in the context of model validation need to be developed. This paper presents a novel methodology for accessing and quantifying validation measurements of radar sensor models. This method uses Light Detection and Rangings (lidars) and the so-called Double Validation Metric (DVM) to effectively quantify deviations between distributions. By applying this metric, the study measures the reproducibility and repeatability of radar sensor measurements. Different interfaces and different levels of detail are investigated. By comparing the radar signals from real-world experiments where different objects are present, valuable insights are gained into the performance of the sensor. In particular, the research extends to assessing the impact of varying rain intensities on the measurement results, providing a comprehensive understanding of the sensor’s behavior under these conditions. This holistic approach significantly advances the evaluation of radar sensor capabilities and enables the quantification of the maximum required quality of radar simulation models.

1. Introduction

Automated driving is one of the biggest challenges facing the automotive industry. Advantages are expected in the areas of connection of village regions, better utilization of existing resources with accompanying minimization of vehicle downtimes, and additional technological development. However, any benefits depend on the safety of such ADFs being proven. Until it is reliable that automation is safer than humans, such systems will not be deployed in large numbers and in all areas of road transport [1]. For a variety of reasons, it is currently not possible to prove safety for such an ADF. One approach that addresses this problem is scenario-based testing [1]. These tests will be performed alongside real test drives in different simulation environments, such as software-in-the-loop, hardware-in-the-loop, or vehicle-in-the-loop. In this way, safety-critical scenarios can be performed for the vehicle and involved agents.
Along with path planning and control, the perception of the environment is an elementary component of ADFs. Therefore, in addition to vehicle dynamics and environment models, sensor models are required to represent the entire ADF pipeline in simulation. However, it is fundamental for the simulation validation process to objectively validate the models used. Both the simulation models and real-world validation measurements play a crucial role in this process. Although the first approaches to validation measurements exist, the comparability, reproducibility, and repeatability of these measurements are often problematic, especially for Radio Detection and Ranging (radar) sensors [2] (p. 68), [3] (p. 84).
In addition to radar, cameras, Light Detection and Ranging (lidar), and ultrasonic sensors are established perception sensors in production vehicles [4]. Radar sensors determine position information, intensities, and speeds by means of frequency modulation, which is determined by the Doppler effect. There are different processing levels in the sensor that can be used for radar sensor model validation measurements. Radar cuboid as a level after a fast Fourier transform (FFT) algorithm in the radar processing chain and detections as a result of the application of dynamic thresholding algorithms [5], which are of interest for this publication. The object list will not be explored further in the course of the paper, as the identification of effects in further processed interfaces increases in complexity.
Therefore, this paper presents a method to compare radar measurements at the radar cuboid and detection levels. The application of this method is intended to provide objective, comparable, and quantifiable radar sensor validation measurements for radar sensor models as part of the safety argumentation of ADFs in the context of scenario-based testing.

1.1. Related Work

There are several measurements in the literature that intend to validate radar models. The related work is separated into radar measurement campaigns as well as lidar and general model validation measurement campaigns.
In order to show the lack of state-of-the-art in this field, the first step is to define the terms repeatability and reproducibility. We define repeatability as the variation of a measurement due to the radar sensor itself. Reproducibility is defined as the variation in the measurement data resulting from the measurement system (setup, sensor, operator) using the same sensor under the same conditions.

1.1.1. Radar

Schaerman et al. transfer real scenarios with a high accuracy of 5 cm standard deviation into the simulation to validate raw data models. However, the repeatability and reproducibility of the measurements are not directly considered [6]. Abadpour presents radar measurements of vulnerable road users and their back-scattering behavior. Nevertheless, the number of repetitions of the measurements is only one trial, and reproducibility is not further addressed [7]. Schneider analyzes different objects and their back-scattering behavior in radar sensors. He compares the characteristics using histograms to investigate the corresponding distributions in the sensor. A deeper investigation about repeatability and reproducibility on radar cuboids and detection levels is missing in his analysis [8]. Eder analyzes an overtaking maneuver with 100 repetitions and finds that the trajectory is almost identical, but the fluctuation and therefore a lack in the repeatability of the measurement result in the detection level hinder a deeper analysis [3]. Holder et al. use EDFs to study the detection distribution of occluded and unoccluded objects. The number of detections on an object is also analyzed using EDFs. Here, three repetitions of the measurement are performed, but a deeper analysis of the repeatability is not considered further [5]. Magosi et al. also aggregate the detections over the bounding box of a scenario but do not consider test repetitions. Only a comparison between simulation and measurement is made [9]. Aust et al. use 10 repetitions of a scenario by driving the radar sensor towards a static object. They aggregate the detections over the bounding box of the target object and examine the distribution of detections using the probability density function (PDF). However, they do not directly compare the measurements with each other [10]. Buddapaggari et al. also use resimulation of measured trajectories to compare detections in over-the-air/vehicle-in-the-loop test beds with real radar data. The number of experimental replicates is also limited to one, which means that measurement repeatability is not further considered [11]. Ngo uses different scenarios to determine the simulation-reality gap he defines for detections and object lists. For each scenario, only one trial repetition is considered [12] (pp. 66, 84). Holder analyzes different scenarios, running three trials for each scenario. Various variations are shown, but in the context of repeatability and reproducibility, these are not discussed further in terms of quantitative deviations and the identification of measurement outliers [2].

1.1.2. Lidar and Other Domains

In addition to radar sensors, different validation measurements of lidar sensors are also introduced in different publications. Rosenberger et al. use a relatively complex validation scenario with multiple objects but also neglect the repeatability of the experiments in their analysis [13]. Linnhoff et al. use a meteorological station to analyze lidar data based on real weather conditions. However, due to the real conditions, there is no reproducibility of the measurements, despite a high number of experimental replicates [14]. In DIN SAE SPEC 91471:2023-05 [15], different measurement setups are presented, which serve for the evaluation of lidar performance. The technical description lacks information about the number of repetitions and an evaluation metric to compare the different results with each other. Viehof uses 15 measurements in the validation of vehicle dynamics models and explicitly emphasizes the need to ensure the quality of the measurement data [16]. However, no specific procedure is given for evaluating the repeatability of the measurements and the deviation quantification.

1.2. Research Questions

The following research questions arise from the validation measurement campaigns in the literature for radar sensors.
Research Question 1: How reproducible are radar measurements and identical measurement setups?
Identical measurements in this case refer to a comparison of unchanged measurement setups in less than 10 min consecutively where the sensor is not switched off. Furthermore, it is investigated how dismantling and reconstruction of the measurement setup behave on the radar measurements at constant position with precise markings on the test track.
Research Question 2: How do different objects and object positions affect radar measurements?
Different objects here denote a corner cube reflector (CCR), which is an ideal point target, and extended targets, which differ in shape and size (Volvo XC90, Mercedes Vito). Furthermore, the poses of the vehicles to the sensor are varied to analyze this influence.
Research Question 3: How do environmental conditions such as rain affect radar validation measurements?
Due to the stochastic behavior of rain, it is challenging to quantify the effect and make different rain intensities comparable.

2. Evaluation Methodology

To answer the research questions, a methodology based on the so-called DVM introduced by Rosenberger [17] (pp. 118,119) is used. The corresponding process is visually illustrated in Figure 1. In the first step, the measurement data for the different experiments is collected. We gather multiple measurements per experiment setup. After pre-processing and position-based filtering of the measurement data, the number of resulting measurement data points is compared between the respective measurements or experiments. We name this filtered area region of interest (ROI). The comparison of the overall number is due to the condition that this deviation must be small for the DVM to be used [17] (p. 103). The DVM is based on a comparison of the EDFs of the measured data and, therefore, the underlying distribution. Rosenberger’s approach uses the area validation metric of Roy et al. [18] (p. 307) and extends it by a second factor to evaluate the EDFs. In contrast to Rosenberger, we do not summarize the individual distribution functions of the measurements, but evaluate the differences of the EDFs individually. Therefore, the area between all the resulting distribution functions is determined, which is a measure for the deviation of the mean value denoted as d bias of the measurements and experiments. Therefore, the mathematical description for d bias results with F denoted as the first EDF, F ˜ denoted as the second EDF, d + denoted as the area between F ˜ and F , where F ˜ F and d denoted as the area between F ˜ and F , where F ˜ < F , in
d bias ( F , F ˜ ) = d d + .
If subsequently the EDFs are shifted by d bias and the resulting area between the corrected EDFs F ˜ c and the first EDF F is calculated, a metric d CAVM for the shape deviation of the distribution functions is obtained, giving information about the scattering difference [17] (pp. 116–119).
Therefore, the following mathematical expression is obtained as
d CAVM ( F , F ˜ ) = d AVM ( F , F ˜ c ) = d c + d c + .
These two parameters give information about the similarity of the different distribution functions in the unit of the analyzed measurand. In a final step, the distribution of d bias and d CAVM is visualized and analyzed via box plots.
Five different evaluation levels are considered input data for the process:
1.
All range azimuth bins with the Doppler component 0 of the radar cuboid → whole radar cuboid (WRC);
2.
All detections in the dimensions distance, azimuth, and Radar Cross Section (RCS) → all detections (WD);
3.
A region of interest, which only includes the bins where the object is present in the measurement, on radar cuboid level with the Doppler component 0 → ROI of the radar cuboid (ROI RC);
4.
A region of interest, which only includes detections where the object is present in the measurement, on detection level → ROI of the detecions (ROI D);
5.
Each range azimuth bin combination separately on the radar cuboid level → each bin of the radar cuboid (EB RC);
The different evaluation levels are selected according to their relative deviation of the number of data points or detections of all measurements for the respective experiment. Furthermore, the additional information content plays a role in whether the evaluation is performed. On this basis, the evaluation scheme in Table 1 is derived, and the evaluation is performed in the following Section 4.

3. Experimental Setup

The validation experiments are performed at the August-Euler airfield in Griesheim. Except for the experiments on Day 1 and Day 2, all experiments are performed with the same sensor position on the airfield. The setup and the orientation of the sensor are very crucial for the analysis of the data because, with effort, the epistemic uncertainties can be reduced and thus increase the comparability between the experiments. The measurement setup consists of a radar sensor mounted on a sensor rack and an object positioned in front of it. The radar sensor is a series of active cruise control (ACC) radars with a maximum range of approx. 200 m. The field of view (FoV) is approx. 12.8 . For each measurement, a measurement time of 60 s is reproduced by the measurement computer. However, due to measurement data failures in the recording, this number may fluctuate.
The frame on which the radar sensor is mounted can be leveled in all directions by means of four adjustable feet. In addition, the height, azimuth angle, and elevation angle of the sensor can be adjusted. The elevation angle is set to 0. The orientation of the azimuth angle of the sensor is set by a centered far point target, and the orientation for the positioning of the point target and the sensor is given by the driving stiff mark. The height is based on the mounting position of the sensor in the vehicle. Therefore, a height of 70 cm is chosen. For the objects, a distinction is made between a point target in the form of a CCR and an extended object in the form of two different vehicles. The vehicles are a Mercedes-Benz Vito (van, production year 2020) and a Volvo XC90 (sport utility vehicle, production year 2019). The chosen objects are exemplars, but the developed methodology is applicable to any kind of object.
The Day 1 and Day 2 experiments do not contain an object. This is to quantify the effects of setup and dismantling, as well as to study the static environment itself. The exact setup of the different experiments can be found in Table 2.
The experimental setup follows the scheme shown in Figure 2. The center of the sensor defines the origin of the drawn S-coordinate system. The object positions are defined relative to this coordinate system. For the description of the experimental setups, a two-dimensional experimental space is chosen, which can be defined by the polar coordinates, distance (r), and azimuth angle ( ϕ ) of the sensor. The reason for this is that the FoV of the sensor is also divided into polar coordinates. As the evaluation is also done at the radar cuboid level, a logical positioning with respect to the bins makes sense. The bins result from the resolution of the sensor in range and azimuth. The real positions of all structures are measured during the experiments with an RTK-based global navigation satellite system (GNSS) antenna. The position of the CCR as a point target is thus described by the two parameters r and ϕ . Due to the size of the vehicles themselves, the position of the vehicle must also be described by the rotation around the vertical axis ψ . For the vehicles, the wheel contact points are measured, and the center of the vehicle and the rotation ψ are calculated accordingly. The direction of rotation of the angles ϕ and ψ is defined in a mathematically positive sense and takes the x-axis of the sensor as a reference.

4. Evaluation

This chapter contains the evaluation results based on the method proposed in Section 2. The chapter is structured as subsections based on the research question’s order.

4.1. RQ 1: Repeatability of Measurements and Reproducibility of Measurement Setups

In the following subsections, five measurements of a CCR are compared with each other to check repeatability (Section 4.1.1). Afterwards, reproducibility is considered on the basis of two sets of eight individual measurements, where the measurements differ in that the sensor is set up and taken down on Day 1. On the following Day 2, the sensor is set up again in the same weather conditions and in as similar a position as possible using markings on the ground (Section 4.1.2).

4.1.1. Comparison of CCR Measurements

In the first step, the number distribution of the five measurements on the different evaluation levels is compared. Figure 3 shows the deviation of the data points. The number of bins from the radar cuboid is nearly identical, with a small deviation of 2 timeframes, corresponding to a percentage deviation of 2.5 ‰. Since the radar cuboid is also used for the evaluation of the ROI and each bin, and it is the same object class for both experiments, the deviation is the same. The number of detections for the whole field of view varies more significantly compared with the data points in the radar cuboid over the different measurements, with a maximum deviation of 11.9 %. Nevertheless, an evaluation of the detections is carried out in the sense of the methodology as an example. For the ROI at the detection level, however, the relative deviations are small, with a maximum of 1.2 ‰.

Whole Radar Cuboid

Figure 4 shows the different EDFs, the box plots for d bias and d CAVM , as well as the number of data points in the different colored distributions. Since the EDFs are very close to each other, it appears in the representation as if only one EDF is shown, whereas the opposite is the case. Due to this closeness, a visualization of the by d bias shifted EDF is omitted.
Both the EDFs and the by d bias corrected EDFs are close to each other, indicating a high degree of agreement between the measured and examined data. The statistical distribution of d bias and d CAVM can be seen in the box plot on the right-hand side of Figure 4. There are only small differences between the five measurements for the two evaluation criteria. Compared to d bias , d CAVM shows a smaller scatter. However, the median of d bias is lower than that of d CAVM . The values obtained show that the spread for d bias is 0.16 dB, while for d CAVM it is only 0.05 dB. In summary, it can be concluded from the analyses carried out that the measurements show high repeatability with respect to the whole radar cuboid. There are no outliers, which means that several successive radar measurements with this sensor can be considered almost identical based on the analysis of the whole radar cuboid.

Whole Detections

In Figure 5 the EDFs and box plots for distance, azimuth, and RCS are visualized. It can be seen that the EDFs for distance are close to each other, but a spread is visible. At a distance of 29.65 m, there is an accumulation of detections, which shows the influence of the CCR. In general, the detections are distributed over a distance of up to 147 m. Close to the sensor, detections are located on the road surface, and with higher distances, the number of detections increases at the transition between vegetation and the road. Furthermore, in the vegetation itself, multiple detections are present. A decrease in the number of detections above 110 m indicates a lower signal-to-noise ratio (SNR), making detections random. Above 147 m, the SNR is so low that there are no more detections in the environment. The median of all d bias is similar to d CAVM in absolute terms. However, the scatter of the d bias values is larger compared with d CAVM . In addition to the very different number of detections and the large scatter in the metrics, the repeatability of the measurement results for the distance of all detections is very low. The influence of the environment is too large to draw conclusions from the distance evaluation.
As with distance, the azimuth distribution is affected by the environment. Between −5 and 5 the CCR is notable with the step at 0. The visible shoulder area next to 0 indicates a few detections due to the road. The second step close to 0 at negative azimuth angles can be associated with detections at close-range as well as at twice the distance between the CCR and the sensor. The median of d bias is about 0.5 , which is a relatively high value in relation to the sensor’s FoV, indicating, in addition to the scatter, a low repeatability of the measurements. The scatter deviation of d CAVM confirms this impression.
The CCR is also evident in the RCS EDFs. 5 % of the detections are due to the point target with an approximate 27 dBm 2 . This indicates high repeatability with respect to the reflectivity characteristics. However, especially for detections at close-range due to asphalt and vegetation, different distributions show the stochastic behavior of the majority of the detections. As before, d bias and d CAVM are difficult to interpret because there is too much randomness in the way the detections are generated by the environment. In particular, there is an outlier in d CAVM , which is due to the comparison of measurements 2 and 5. Here, the number of detections is the most spread over all measurements.
From the evaluation of all detections, it can be concluded that a comparison of all detections is not useful for the validation of this specific radar sensor. The environment has too much influence on the detection distribution. This evaluation experiment can be used in future validation studies to assess whether an evaluation of all detections is useful in the studied environment in the context of validation measurements.

ROI Radar Cuboid

Figure 6 shows the same structure as in the previous evaluations. However, in this case, only the bin of the radar cuboid and therefore the power where the CCR is located are analyzed. The distribution functions show a slight deviation from each other. This is also reflected in the two metrics. The deviations in d bias show a spread of 0.045 dB and a much smaller spread in d CAVM . This shows that the repeatability of the experiments for the CCR is even higher in comparison to the whole radar cuboid. This evaluation is therefore suitable for validation measurements in the case of this sensor for point targets.

ROI Detections

Figure 7 visualizes the RCS distribution of the CCR detections based on an ROI. Due to the point target characteristics and the small, defined ROI, an analysis of the distance and azimuth is not discussed. The deviations in d bias are 0.01 dbm 2 , and an even smaller scatter in d CAVM appears. Finally, the ROI on detection level shows a high repeatability of the measurements. For point targets, it can therefore be concluded that a ROI can be used as a filter on the detection level for validation measurements.

Each Range and Azimuth Bin on Radar Cuboid Level

For a detailed analysis of the environmental influence on the repeatability of the radar cuboid, the EDFs are compared using d bias and d CAVM for each individual range azimuth bin. For this purpose, the respective maximum of | d bias | and d CAVM of the corresponding range azimuth bin are visualized with a satellite image and the radar position measured by the GNSS sensor. This makes it possible to interpret the causes of anomalies and assign them to areas in the radar FoV. The result is shown in Figure 8.
It can be seen that for the CCR position, there are small deviations across all azimuths and ± 2 range bins. This can be explained by the results of the ROI of the CCR. Due to the high back scattering power, stochastic effects are less pronounced. Due to the window functions used in the radar sensor, the power is smeared into the neighboring bins of the radar cuboid, resulting in the high repeatability in the previously identified range for d bias and d CAVM . Only in front of and behind this area do deviations occur in both metrics in the center of the FoV. In the near range, the largest deviations occur for d bias and d CAVM . These variations in the radar cuboid lead to the close-range detections identified in the whole detection analysis. In general, the transition from road to vegetation causes the largest deviations. Here, the deviations decrease with increasing azimuth space from the grass. The road surface, on the other hand, shows a very high repeatability of the measurements, with only minor deviations. Cracks and vegetation on the runway are possible explanations for this observation. Smaller deviations at the road junction confirm this impression when the opposite side with the grass is also taken into account. As the distance increases, the deviations in the two metrics decrease, and the distributions in the different cells become more similar.

4.1.2. Dismantling and Setting Up on Two Different Days

In this chapter, measurement data from two consecutive days with eight measurements each is compared. No object is placed in front of the radar sensor, and only the surrounding area is measured. A dismantling and reassembly of the measurement setup between the two days is performed. In this way, the reproducibility of the radar model validation measurement setup is checked, and the second part of RQ 1 is addressed. Compared to the CCR measurements, the sensor position on the runway is different, but this does not affect the research objective.
In itself, the measurements between Day 1 and Day 2 are consistent in terms of the number of data points (see Figure 9). However, it can be seen that switching the sensor and PC on and off for data recording has an effect on the number of data points. The recording time is always 60 s for both days. It follows that such effects must be taken into account in the quality assurance of the measured data for the validation of sensor models. Due to the fact that no objects were placed, an analysis of the ROI RC and the ROI D is not feasible.

Whole Radar Cuboid

In general, the EDFs of the whole radar cuboid are visually close, which is confirmed by the deviations in d bias and d CAVM (see Figure 10). However, a comparison of these measurements with those of CCR shows that the scatter of d bias and d CAVM is greater.
To support this observation, Figure 11 shows the comparison of d bias and d CAVM for Day 1/2, Day 1/1 and Day 2/2. It can be seen that reconfiguring the measurement setup has a greater effect than taking several measurements in succession. With the method presented, this effect is quantifiable via the scatter of the two metrics, and the reproducibility is measurable.

Each Range and Azimuth Bin on Radar Cuboid Level

Figure 12 shows d bias and d CAVM over all range azimuth bins. The largest deviations occur in the near range of the sensor, with up to a 15 dB difference in power for d bias at the edge of the FoV. Compared to the CCR measurements, where only 5 dB are present. It can be concluded that the close-range is particularly affected by the mounting and dismounting of the sensor. Especially for validation measurements with objects and environments, the reproducibility of the measurements must be checked before using them for a validity statement. For this reason, close-range measurements must be taken with particular accuracy. On the road surface, deviations of up to 10 dB in d bias can be detected up to a distance of 74 m. The roadside, on the other hand, has an effect on the readings over the whole visibility range due to differences in the sensor orientation. Both d bias and d CAVM show deviations at identical positions in the range azimuth map.

4.2. RQ 2: Effects of Objects on Radar Measurements

In this chapter, the influence of objects on radar validation measurements is investigated. For this purpose, the measurements of the CCR from Section 4.1.1 are first compared with those of a Volvo XC90. The center of the vehicle is almost identical to the position of the CCR. The yaw angle of the vehicle is close to 0. Next, the XC90 is observed in the identical position but rotated by a yaw angle in the second experiment. This analyzes the influence of the rotation on the measurement result. Finally, the XC90 and a Mercedes Vito are compared with each other at an almost identical position and yaw angle.

4.2.1. Comparison of the CCR and XC90

In this chapter, effects due to complex geometries compared with an ideal target are identified. Figure 13 shows the number of data points between detection and radar cuboid level. The relative deviation for the radar cuboid level is for the evaluation of WRC, the ROI RC, and the EB RC, which are similar and below 1%. At the detection level, the number of detections differs significantly between the objects, which is why a comparison for the evaluation of WD and the ROI D is not meaningful.

Whole Radar Cuboid

Figure 14 visualizes the result for the comparison of the vehicle and the ideal target. For the entire radar cuboid, it is evident from the EDFs that the CCR affects all bins. Already at −82 dB deviations are recognizable. At occurrences above 90%, the EDF of both objects equalizes again. At −78 dB, there is a kink in the course of the EDF of the XC90, which suggests the influence of the environment, since this kink is also evident in the measurements of Day 1/2. For d bias , a median of −2 dB is shown for the whole radar cuboid. The different shape of the EDF is also reflected in d CAVM . The values have significantly increased compared with the previous experiments.

Each Range and Azimuth Bin on Radar Cuboid Level

The analysis of the data in Figure 15 shows significant differences in d bias , especially at the object positions. These discrepancies can be attributed to the better reflective properties of the CCR. In addition, the influence of the windowing function can be seen, which smears the power across the range bins. This effect is noticeable in the central area of the FoV. The deviations at the edge of the roadway again confirm the effect already described in the evaluation of the entire radar cuboid. The CCR influences all bins. This finding is also reflected in the distribution of the d CAVM . Lower deviations are seen both at the object’s position and at twice the distance. This is a proof of the reproducibility of multipath propagation of radar waves due to objects. In general, it can be seen that the object is influenced by its surrounding and its characteristics.

4.2.2. Comparison of XC90 and Rotated XC90

In this section, the rotation of an object on the wave propagation for an exemplary yaw angle is examined. However, the difference between these two experiments is the yaw angle of the same object. As in Section 4.2.1, the relative deviation on the detection level is significantly higher than the deviation o then radar cuboid level. Due to the high deviations on the detection level, see Figure 16, the comparability of the measurements and thus of the experiments is not given. Therefore, this comparison is only evaluated at the radar cuboid level. The relative deviations on the radar cuboid level for the different evaluations (WRC, ROI RC, and EB RC) are in the same order of magnitude and thereby below 1%.

Whole Radar Cuboid

The rotation of the object has a small influence on the total power distribution in the radar cuboid, as visible in Figure 17. The distribution functions are again visually hardly separable, which is reflected in the values for d bias and d CAVM . The scatter of d bias is 0.17 dB, which puts the difference in a range also observed in the CCR measurements. This can be explained by the main influence of the environment and the disproportionate amount of road and vegetation in the measurements. An effect over the entire radar cuboid due to rotation, as in the CCR and XC90 comparisons, cannot be observed. Based on this finding, an evaluation of the whole detection is omitted, and a detailed look at the ROI is given.

ROI Radar Cuboid

The evaluation of the ROI is shown in Figure 18. The rotation leads to a significant decrease in the power values in the filtered bins, with little fluctuation between experiments. This observation confirms d bias with a significant deviation of 5.5 dB at the median. Rotation also affects the shape of the distribution functions, such that d CAVM is almost equal to 2.8 dB. The results show high inter-experiment repeatability for static experiments but a significant influence of object orientation.

Each Range and Azimuth Bin on Radar Cuboid Level

The findings from the ROI become even clearer in the satellite image (see Figure 19). Especially in the vicinity of the object, values of 25 dB are present in d bias . In this area, however, d CAVM shows only low values, which speaks for the previously established high repeatability of the results in this area. Interesting are the high deviations in d bias at the roadside and partly in the vegetation. 15 dB are increasingly and patchily detectable. This is further evidence of the influence of objects on the detected surroundings due to multipath propagation or effects in the signal processing of the radar sensor. The variations of d CAVM are largest where d bias is also high. Comparison with satellite images of CCR and XC90 shows similar values, suggesting a stochastically constant behavior of vegetation in the different experiments and measurements.

4.2.3. Comparison of Volvo XC90 and Mercedes Vito

Finally, the Volvo XC90 is compared with a Mercedes Vito. The effects of different object geometries and sizes are analyzed regarding their effects on validation measurement campaigns. The relative deviations are comparable to the previous findings. The deviations are higher at the detection level than those at the radar cuboid level, as seen in Figure 20. However, there is a difference in the deviations of all detections compared with the deviations for the detections in the ROI, which are significantly higher. Thus, also for this comparison, an evaluation is performed on the radar cuboid level with a relative deviation for the number of data points below 1 % and the whole detections.

Whole Radar Cuboid

Furthermore, the entire radar cuboid is analyzed. From Figure 21, it can be seen that the object has an influence on all bins, as in the comparison of CCR and XC90. This can be seen from the higher power distribution of the EDFs in the Mercedes Vito. The shape of the object (hatchback compared with vertical rear) therefore has a direct influence on the measured environment. In addition to the rear, the underbody can also influence the measurement result. The overall effect can be seen in d bias , which shows a relatively high deviation with a low spread. For both metrics, it can be seen that the repeatability of the measurements of the different objects is very high, as the scatter is low.

Whole Detections

Figure 22 shows the EDFs for the distance, azimuth, and RCS, as well as a corresponding box plot for them. A look at the EDFs for the distance shows that these are similar to each other, but a deviation is still visible. In the distance of the vehicles at 29.65 m, a small step and thus an accumulation of detections can be seen. All detections extend over a maximum distance of 150 m. In the vicinity of the sensor, these detections result from reflections of the road surface and, with increasing distance, from the transition between road and vegetation. Whereby it can be seen from the course that at distances over 115 m, fewer detections can be recognized. Above 160 m, only isolated detections with a low RCS are present, which argues for purely stochastic causes. The median values for d bias and d CAVM are similar when considered as absolute values. However, the scatter of d bias at 5 m is significantly larger than the scatter of d CAVM at 1 m.
Looking at the EDFs for the azimuth, it is noticeable that the EDFs overlap better for angles below 0 than for angles above 0. Furthermore, the steps for the accumulation of detections by the two vehicles are different, so the step for the XC90 is at 1.5 and not as significant as the one for the Vito at 0. Basically, however, there is an accumulation of detections around 0 for both vehicles, which corresponds to the vehicle position and reflections from the road surface near the sensor. For angles below −5 and above 5 , detections can be seen by the transition from the road surface to vegetation. The plateaus between −5 and 0, and between 0 and 5 , are due to the road surface. The median values of d bias and d CAVM are similar for an absolute observation. However, it can again be seen that the scatter is larger for the d bias than for the d CAVM .
When looking at the EDFs for the RCS, these are close to the two vehicles between −30 dBm 2 and −10 dBm 2 and have a similar trend, but a deviation is visible. Below −30 dBm 2 , the EDFs of the XC90 are determined by more significant steps compared with the Vito. Above −10 dBm 2 , the curve is similar, but there is a clear offset between the two vehicles, indicating more detections on the Vito, proving the findings in Figure 20. The steps above −10 dBm 2 indicates the RCS for both vehicles. A difference in the maximum RCS for the detections can be observed; the RCS for the XC90 is 5 dBm 2 less than the RCS of the Vito. In addition, a difference in the number of detections between the XC90 and the Vito can be seen in the level of the step. The medians for d bias and d CAVM differ by 1.75 dBm 2 , with this being larger for d CAVM . However, the dispersion for d bias is 0.2 dBm 2 larger than for d CAVM . As noted in the comparison of the two CCRs, it is difficult to interpret the d bias and d CAVM due to the randomness that comes from the vegetation-generated detections.

ROI Radar Cuboid

Figure 23 shows the ROI at the radar cuboid level. It confirms the impression from the analysis of all bins of the radar cuboid. In general, the Vito generates more power in the bins around its own position. Thereby, a high level of repeatability between the individual measurements is shown. The outer bins of the ROI provide the low powers, which are similar for both objects. However, d bias also increases with increasing power values. d bias shows values from 3.7 dB to 3.95 dB and illustrates the deviations caused by the object geometry. Similarly, d CAVM is clearly influenced by the different objects. Therefore, the shape of the distribution functions differs because of the different objects.

Each Range and Azimuth Bin on Radar Cuboid Level

The detailed analysis of the range of azimuth bins is visualized in Figure 24. For d bias , it is clearly visible that there are increased deviations in front of and behind the vehicle position. These extend over the entire azimuth range and are up to 18 dB in the center. At twice the vehicle distance, multipath propagation across the sensor is evident. These are the largest at up to 25 dB and also extend over the entire azimuth range due to the windowing function. There is also a deviation up to maximum visibility in the center of the FoV. This effect is more noticeable in the comparison between the CCR and the XC90. Here, the higher reflectivity of the Vito causes smearing in the more distant-range bins due to the sensor’s windowing functions. For d CAVM there are increased values in the double distance in the object position as well as for vegetation, which is comparable to the satellite images of the other object analyses.

4.3. RQ3: Influence of Rain on Radar Measurements

For the experiment, the XC90 is in the same position, but five measurements are recorded without rain and five measurements with rain. Subjectively, the intensity of the rain decreases over time.
The rain is of natural origin, and no rain intensity or raindrop size distribution data are available.
Also for the investigation of the environmental conditions, in this case rain, a difference of the relative deviations for the number of data points is shown (see Figure 25). On the detection level, the deviation is higher than on the radar cuboid level. However, the deviations for the evaluation of all detections are many times higher than those for the detections from the ROI. The rain increases the number of detections. Therefore, the evaluation is examined at the radar cuboid level. The relative deviation is similar for every evaluation on the radar cuboid level and below 1%.

4.3.1. Whole Radar Cuboid

In Figure 26, the EDFs of the whole radar cuboid are shown. Rain generally increases the power of all bins. The rain measurement No. 5 lays on the measurements without rain. This may be due to the fact that the rain intensity in this measurement is already low. There is no reference data for rain intensity to make an accurate assessment. From −70 dB, the curves of all EDFs equalize, which shows the increasing influence of the XC90. This is again evident in the box plots for d bias and d CAVM . Rain leads to larger deviations in both metrics compared with the previous measurements in Section 4.2. For a detailed analysis, the satellite image is used.

4.3.2. Each Range and Azimuth Bin on Radar Cuboid Level

The satellite image in Figure 27 clearly shows the effect of the rain. The increased power is shown in both d bias and d CAVM . In particular, d bias is increased in the vicinity of the sensor and up to about half of the FoV. The road surface is particularly affected by this phenomenon. For d CAVM , the largest deviations occur in the medium range of the FoV. Furthermore, the road is more affected than the vegetation, which can be explained by the previously identified stochastic properties of the vegetation.

5. Conclusions

This paper presents a methodology to make radar measurements comparable in the context of the validation of radar sensor models. The two metrics d bias and d CAVM are used to evaluate the similarity of the measured distribution functions. For this purpose, the number of data points is first analyzed in order to be able to make any comparisons using DVM. The analysis of the level of the radar cuboid simplifies the explanation of the different effects, especially in combination with the representation of the range azimuth bins using a satellite image. Finally, the research questions raised in Section 1.2 are answered, and the applicability of the findings to other radar sensors remains to be shown.
Research Question 1: The analysis of the measurements with a CCR shows in direct comparison that there is good repeatability of the measurements, especially near an object in radar measurements. Only vegetation and the road surface in close proximity are characterized by larger deviations in d bias and d CAVM . Furthermore, the dismantling and repositioning shows that smaller influences occur. Nevertheless, the measurements can be performed reproducibly with the right tools (e.g., ground markers).
Research Question 2: Extended objects can be analyzed in detail with the presented methodology, and deviations can be quantified accordingly. However, it can be seen that objects have a direct impact on the overall FoV of the sensor, depending on the orientation and type of object.
Research Question 3: Based on our methodology, environmental influences are comparable, and their influence is quantitatively detectable. In particular, the close-range of the radar sensor shows larger deviations due to rain on average. With increasing distance, rain leads to larger scattering, whereas the effect decreases again after a certain distance and the rain merges with the background noise of the sensor.
Therefore, for validation measurements of radar sensors, the following aspects can be derived from the results:
  • Measurements of static vehicles and point targets are well reproducible on radar cuboid and detection levels.
  • Vegetation and the close-range of the radar sensor lead to large deviations, especially on the detection level, which is why this interface complicates the validation of radar sensor models with the methodology described here.
  • The presented methodology can be used to quantify deviations between validation measurements and identify measurement outliers.
  • Using ideal laboratory measurements, effects in real measurements can be identified based on the deviations in d bias and d CAVM , and their influence can also be quantified (e.g., multipath propagation and interference).
  • With the presented methodology, a maximum achievable quality of simulation models can be determined with a quantitative value in the unit of the measurand with respect to the repeatability and reproducibility of experiments.
The previous considerations refer only to static scenarios. In particular, dynamic tests are of great importance for the radar sensor due to the Doppler effect and the associated direct velocity measurement. Therefore, in the next step, the approach and analysis will be transferred to dynamic scenarios. So far, only the usefulness of the methodology for the sensor used has been demonstrated. In the next step, the knowledge gained has to be proven with other radar sensors.

Author Contributions

Conceptualization, L.E.; methodology, L.E.; software, L.E. and J.P.S.; validation, L.E. and J.P.S.; formal analysis, L.E.; investigation, L.E. and J.P.S.; data curation, L.E.; writing—original draft preparation, L.E. and J.P.S.; writing—review and editing, L.E., J.P.S. and S.P.; supervision, S.P. All authors have read and agreed to the published version of the manuscript.

Funding

This research was funded by the German Federal Ministry for Education and Research (BMBF) through the project Virtual Validation Tool Chain for Automated and Connected Driving (VIVID) under grant number 16ME0173.

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

Data sharing is not applicable to this article.

Conflicts of Interest

The authors declare no conflict of interest.

Abbreviations

The following abbreviations are used in this manuscript:
ACCactive cruise control
ADFautomated driving function
CCRcorner cube reflector
Ddetecions
DVMDouble Validation Metric
EB RCeach bin of the radar cuboid
EDFempirical cumulative distribution function
FFTfast Fourier transform
FoVfield of view
GNSSglobal navigation satellite system
Lidarlight detection and ranging
PDFprobability density function
RadarRadio Detection and Ranging
RCradar cuboid
RCSRadar Cross Section
RTKreal time kinematic
ROIregion of interest
SNRsignal-to-noise ratio
WDwhole detections
WRCwhole radar cuboid

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Figure 1. Used Methodology for the comparison of different experiment setups (E1 and E2), measurements and input data on radar cuboid as well as detection level.
Figure 1. Used Methodology for the comparison of different experiment setups (E1 and E2), measurements and input data on radar cuboid as well as detection level.
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Figure 2. On the left side a sketch of the experimental setup is shown. The Cartesian sensor coordinate system origin is denoted as S x and S y . The parameters for the different experiments are the polar coordinates distance r and azimuth angle ϕ . The yaw angle of the object is defined as ψ . On the right side a picture of the measurement setup of the XC90 on the August-Euler airfield is visualized.
Figure 2. On the left side a sketch of the experimental setup is shown. The Cartesian sensor coordinate system origin is denoted as S x and S y . The parameters for the different experiments are the polar coordinates distance r and azimuth angle ϕ . The yaw angle of the object is defined as ψ . On the right side a picture of the measurement setup of the XC90 on the August-Euler airfield is visualized.
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Figure 3. Plot of the relative deviation for the number of the data points or detections of all measurements of the CCR experiment. The evaluation is shown for the WRC, WD, the ROI RC and the ROI D, as well as EB RC. The gradations of the respective color delineate the different measurements.
Figure 3. Plot of the relative deviation for the number of the data points or detections of all measurements of the CCR experiment. The evaluation is shown for the WRC, WD, the ROI RC and the ROI D, as well as EB RC. The gradations of the respective color delineate the different measurements.
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Figure 4. EDFs of all five measurements of the CCR on the radar cuboid level. The number of aggregated bins is listed below the diagram. On the right side the box plot for d bias and d CAVM is shown.
Figure 4. EDFs of all five measurements of the CCR on the radar cuboid level. The number of aggregated bins is listed below the diagram. On the right side the box plot for d bias and d CAVM is shown.
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Figure 5. EDFs of all five measurements of the CCR on the detection level. In the first row the distance distribution, in the second row the azimuth distribution and in the third row the RCS distribution with the corresponding box plot for d bias and d CAVM are shown. The aggregated number of detections is listed below the diagrams.
Figure 5. EDFs of all five measurements of the CCR on the detection level. In the first row the distance distribution, in the second row the azimuth distribution and in the third row the RCS distribution with the corresponding box plot for d bias and d CAVM are shown. The aggregated number of detections is listed below the diagrams.
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Figure 6. EDFs of all five measurements of the CCR on the radar cuboid level filterd by an ROI are shown in the diagram. The power distribution with the corresponding box plot for d bias and d CAVM is visualized on the right side. The aggregated number of bins is listed below the diagram.
Figure 6. EDFs of all five measurements of the CCR on the radar cuboid level filterd by an ROI are shown in the diagram. The power distribution with the corresponding box plot for d bias and d CAVM is visualized on the right side. The aggregated number of bins is listed below the diagram.
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Figure 7. EDFs of all five measurements of the CCR on the detection level filterd by an ROI are shown in the diagram. The RCS distribution with the corresponding box plot for d bias and d CAVM is visualized on the right side. The aggregated number of detections of all timeframes is listed below the diagram.
Figure 7. EDFs of all five measurements of the CCR on the detection level filterd by an ROI are shown in the diagram. The RCS distribution with the corresponding box plot for d bias and d CAVM is visualized on the right side. The aggregated number of detections of all timeframes is listed below the diagram.
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Figure 8. Satellite image fused with | d bias | and d CAVM coded in colors for each range azimuth bin. The red circle visualizes the position of the CCR.
Figure 8. Satellite image fused with | d bias | and d CAVM coded in colors for each range azimuth bin. The red circle visualizes the position of the CCR.
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Figure 9. Plot of the relative deviation for the number of the data points or detections of all measurements of the two test days, Day 1 and Day 2. The compared data are WRC, the ROI for the ROI RC and EB RC. Experiment 1 is denoted as Applsci 13 11405 i001 and experiment 2 as Applsci 13 11405 i002. The gradations of the respective color delineate the different measurements.
Figure 9. Plot of the relative deviation for the number of the data points or detections of all measurements of the two test days, Day 1 and Day 2. The compared data are WRC, the ROI for the ROI RC and EB RC. Experiment 1 is denoted as Applsci 13 11405 i001 and experiment 2 as Applsci 13 11405 i002. The gradations of the respective color delineate the different measurements.
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Figure 10. EDFs of all eight measurements for Day1 (Applsci 13 11405 i003) and Day 2 (Applsci 13 11405 i004) each on the radar cuboid level. The number of aggregated bins is listed below the diagram. On the right side the box plot for d bias and d CAVM in dB is shown.
Figure 10. EDFs of all eight measurements for Day1 (Applsci 13 11405 i003) and Day 2 (Applsci 13 11405 i004) each on the radar cuboid level. The number of aggregated bins is listed below the diagram. On the right side the box plot for d bias and d CAVM in dB is shown.
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Figure 11. Comparison of d bias and d CAVM based on the whole radar cuboid for Day 1/2, Day 1/1, and Day 2/2. The repeatability between the measurements of each day is higher than the reproduciblity of the measurement setup.
Figure 11. Comparison of d bias and d CAVM based on the whole radar cuboid for Day 1/2, Day 1/1, and Day 2/2. The repeatability between the measurements of each day is higher than the reproduciblity of the measurement setup.
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Figure 12. Satellite image fused with | d bias | and d CAVM coded in colors for each range azimuth bin.
Figure 12. Satellite image fused with | d bias | and d CAVM coded in colors for each range azimuth bin.
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Figure 13. Plot of the relative deviation for the number of the data points or detections of all measurements of the two experiments (CCR and XC90). All evaluation levels are compared. Experiment 1 is denoted as Applsci 13 11405 i001 and experiment 2 as Applsci 13 11405 i002. The gradations of the respective color delineate the different measurements.
Figure 13. Plot of the relative deviation for the number of the data points or detections of all measurements of the two experiments (CCR and XC90). All evaluation levels are compared. Experiment 1 is denoted as Applsci 13 11405 i001 and experiment 2 as Applsci 13 11405 i002. The gradations of the respective color delineate the different measurements.
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Figure 14. EDFs of all five measurements for the objects CCR (Applsci 13 11405 i005) and the Volvo XC90 (Applsci 13 11405 i006) each on the radar cuboid level. The number of aggregated bins is listed below the diagram. On the right side the box plot for d bias and d CAVM in dB is shown.
Figure 14. EDFs of all five measurements for the objects CCR (Applsci 13 11405 i005) and the Volvo XC90 (Applsci 13 11405 i006) each on the radar cuboid level. The number of aggregated bins is listed below the diagram. On the right side the box plot for d bias and d CAVM in dB is shown.
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Figure 15. Satellite image fused with | d bias | and d CAVM coded in colors for each range azimuth bin. The objects under examination are a CCR and a Volvo XC90. The red circle visualizes the position of both objects.
Figure 15. Satellite image fused with | d bias | and d CAVM coded in colors for each range azimuth bin. The objects under examination are a CCR and a Volvo XC90. The red circle visualizes the position of both objects.
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Figure 16. Plot of the relative deviation for the number of the data points of all measurements of the two experiments (XC90 and XC90 rotated).The WRC, WD, the ROI for the ROI RC and the ROI D, as well as EB RC are compared. Experiment 1 is denoted as Applsci 13 11405 i001 and experiment 2 as Applsci 13 11405 i002. The gradations of the respective color delineate the different measurements.
Figure 16. Plot of the relative deviation for the number of the data points of all measurements of the two experiments (XC90 and XC90 rotated).The WRC, WD, the ROI for the ROI RC and the ROI D, as well as EB RC are compared. Experiment 1 is denoted as Applsci 13 11405 i001 and experiment 2 as Applsci 13 11405 i002. The gradations of the respective color delineate the different measurements.
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Figure 17. EDFs of all five measurements for the XC90 (Applsci 13 11405 i007) and the XC90 rotated (Applsci 13 11405 i008) each on the radar cuboid level. The number of aggregated bins is listed below the diagram. On the right side the box plot for d bias and d CAVM in dB is shown.
Figure 17. EDFs of all five measurements for the XC90 (Applsci 13 11405 i007) and the XC90 rotated (Applsci 13 11405 i008) each on the radar cuboid level. The number of aggregated bins is listed below the diagram. On the right side the box plot for d bias and d CAVM in dB is shown.
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Figure 18. EDFs of all five measurements of the XC90 (Applsci 13 11405 i009) and the rotated XC90 (Applsci 13 11405 i010) on the radar cuboid level filterd by an ROI are shown in the diagram. The power distribution with the corresponding box plot for d bias and d CAVM is visualized on the right side. The aggregated number of bins is listed below the diagram.
Figure 18. EDFs of all five measurements of the XC90 (Applsci 13 11405 i009) and the rotated XC90 (Applsci 13 11405 i010) on the radar cuboid level filterd by an ROI are shown in the diagram. The power distribution with the corresponding box plot for d bias and d CAVM is visualized on the right side. The aggregated number of bins is listed below the diagram.
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Figure 19. Satellite image fused with | d bias | and d CAVM coded in colors for each range azimuth bin. The object under examination is a Volvo XC90 with different yaw angles. The red circle visualizes the center of the vehicle’s bounding box.
Figure 19. Satellite image fused with | d bias | and d CAVM coded in colors for each range azimuth bin. The object under examination is a Volvo XC90 with different yaw angles. The red circle visualizes the center of the vehicle’s bounding box.
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Figure 20. Plot of the relative deviation for the number of the data points of all measurements of the two experiments (XC90 and Vito). The WRC, WD, the ROI for the ROI RC and the ROI D, as well as EB RC are visualized. Experiment 1 is denoted as Applsci 13 11405 i001 and experiment 2 as Applsci 13 11405 i002. The gradations of the respective color delineate the different measurements.
Figure 20. Plot of the relative deviation for the number of the data points of all measurements of the two experiments (XC90 and Vito). The WRC, WD, the ROI for the ROI RC and the ROI D, as well as EB RC are visualized. Experiment 1 is denoted as Applsci 13 11405 i001 and experiment 2 as Applsci 13 11405 i002. The gradations of the respective color delineate the different measurements.
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Figure 21. EDFs of all five measurements for the Volvo XC90 (Applsci 13 11405 i011) and the Mercedes Vito (Applsci 13 11405 i012) each on the radar cuboid level. The number of aggregated bins is listed below the diagram. On the right side the box plot for d bias and d CAVM in dB is shown.
Figure 21. EDFs of all five measurements for the Volvo XC90 (Applsci 13 11405 i011) and the Mercedes Vito (Applsci 13 11405 i012) each on the radar cuboid level. The number of aggregated bins is listed below the diagram. On the right side the box plot for d bias and d CAVM in dB is shown.
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Figure 22. EDFs of all five measurements of the XC90 (Applsci 13 11405 i013) and Vito (Applsci 13 11405 i014) on the detection level. In the first row the distance distribution, in the second row the azimuth distribution and in the third row the RCS distribution with the corresponding box plot for d bias and d CAVM are shown. The aggregated number of detections is listed below the diagrams.
Figure 22. EDFs of all five measurements of the XC90 (Applsci 13 11405 i013) and Vito (Applsci 13 11405 i014) on the detection level. In the first row the distance distribution, in the second row the azimuth distribution and in the third row the RCS distribution with the corresponding box plot for d bias and d CAVM are shown. The aggregated number of detections is listed below the diagrams.
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Figure 23. EDFs of all five measurements of the Volvo XC90 (Applsci 13 11405 i015) and Mercedes Vito (Applsci 13 11405 i016) on the radar cuboid level filterd by an ROI are shown in the diagram. The power distribution with the corresponding box plot for d bias and d CAVM is visualized on the right side. The aggregated number of bins is listed below the diagram.
Figure 23. EDFs of all five measurements of the Volvo XC90 (Applsci 13 11405 i015) and Mercedes Vito (Applsci 13 11405 i016) on the radar cuboid level filterd by an ROI are shown in the diagram. The power distribution with the corresponding box plot for d bias and d CAVM is visualized on the right side. The aggregated number of bins is listed below the diagram.
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Figure 24. Satellite image fused with d bias and d CAVM coded in colors for each range azimuth bin. The object under examination is a Volvo XC90 and a Mercedes Vito at the same position and orientation. The red circle visualizes the center of the vehicles’ bounding boxes.
Figure 24. Satellite image fused with d bias and d CAVM coded in colors for each range azimuth bin. The object under examination is a Volvo XC90 and a Mercedes Vito at the same position and orientation. The red circle visualizes the center of the vehicles’ bounding boxes.
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Figure 25. Plot of the relative deviation for the number of the data points of all measurements of the two experiments (XC90 and XC90 with rain). The WRC, WD, the ROI for the ROI RC and the ROI D, as well as EB RC are compared. Experiment 1 is denoted as Applsci 13 11405 i001 and experiment 2 as Applsci 13 11405 i002. The gradations of the respective color delineate the different measurements.
Figure 25. Plot of the relative deviation for the number of the data points of all measurements of the two experiments (XC90 and XC90 with rain). The WRC, WD, the ROI for the ROI RC and the ROI D, as well as EB RC are compared. Experiment 1 is denoted as Applsci 13 11405 i001 and experiment 2 as Applsci 13 11405 i002. The gradations of the respective color delineate the different measurements.
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Figure 26. EDFs of five measurements of the XC90 in dry (Applsci 13 11405 i017) and rainy (Applsci 13 11405 i018) conditions on the radar cuboid level. The number of aggregated bins is listed below the diagram. On the right side the box plot for d bias and d CAVM in dB is shown.
Figure 26. EDFs of five measurements of the XC90 in dry (Applsci 13 11405 i017) and rainy (Applsci 13 11405 i018) conditions on the radar cuboid level. The number of aggregated bins is listed below the diagram. On the right side the box plot for d bias and d CAVM in dB is shown.
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Figure 27. Satellite image fused with | d bias | and d CAVM coded in colors for each range azimuth bin. The object under examination is a Volvo XC90 in rainy and dry conditions. The red circle visualizes the center of the vehicle bounding box.
Figure 27. Satellite image fused with | d bias | and d CAVM coded in colors for each range azimuth bin. The object under examination is a Volvo XC90 in rainy and dry conditions. The red circle visualizes the center of the vehicle bounding box.
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Table 1. Overview of the application of the different evaluation levels. In the first column, the compared experiments and objects are listed, which are explained in detail in Section 3.
Table 1. Overview of the application of the different evaluation levels. In the first column, the compared experiments and objects are listed, which are explained in detail in Section 3.
ExperimentWRCWDROI RCROI DEB RC
CCR\ CCRXXXXX
Day 1\ Day 2X X
CCR\ XC90X X
XC90\ XC90 rotatedX X X
XC90\ VitoXXX X
XC90\ XC90 rainX X
Table 2. Different parameters in the experimental setups. In the first column the compared objects are listed with the corresponding parameters.
Table 2. Different parameters in the experimental setups. In the first column the compared objects are listed with the corresponding parameters.
Experimentr in m ϕ in ψ in
CCR\CCR29.56\29.560\00\0
Day 1\Day 2---
CCR\XC9029.56\29.500\00\0.5
XC90\XC90 rotated29.50\29.680\0.10.5\13.7
XC90\Vito29.50\29.590\00.5\−0.2
XC90 \XC90 rain48.60\48.608.1\8.1−1.1\−1.1
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Elster, L.; Staab, J.P.; Peters, S. Making Automotive Radar Sensor Validation Measurements Comparable. Appl. Sci. 2023, 13, 11405. https://doi.org/10.3390/app132011405

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Elster L, Staab JP, Peters S. Making Automotive Radar Sensor Validation Measurements Comparable. Applied Sciences. 2023; 13(20):11405. https://doi.org/10.3390/app132011405

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Elster, Lukas, Jan Philipp Staab, and Steven Peters. 2023. "Making Automotive Radar Sensor Validation Measurements Comparable" Applied Sciences 13, no. 20: 11405. https://doi.org/10.3390/app132011405

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