# Measurement of Rank and Other Properties of Direct and Scattered Signals

Authors: Svante Björklund; Per Grahn; Anders Nelander; Mats I. Pettersson
Journal: International Journal of Antennas and Propagation
 (2016)

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## Abstract

We have designed an experiment for low-cost indoor measurements of rank and other properties of direct and scattered signals with radar interference suppression in mind. The signal rank is important also in many other applications, for example, DOA (Direction of Arrival) estimation, estimation of the number of and location of transmitters in electronic warfare, and increasing the capacity in wireless communications. In real radar applications, such measurements can be very expensive, for example, involving airborne radars with array antennas. We have performed the measurements in an anechoic chamber with several transmitters, a receiving array antenna, and a moving reflector. Our experiment takes several aspects into account: transmitted signals with different correlation, decorrelation of the signals during the acquisition interval, covariance matrix estimation, noise eigenvalue spread, calibration, near-field compensation, scattering in a rough surface, and good control of the influencing factors. With our measurements we have observed rank, DOA spectrum, and eigenpatterns of direct and scattered signals. The agreement of our measured properties with theoretic and simulated results in the literature shows that our experiment is realistic and sound. The detailed description of our experiment could serve as help for conducting other well-controlled experiments.


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## Body

## 1. Introduction

In this article we have designed an experiment for low-cost indoor measurements of rank and other properties of direct and scattered signals with radar applications in mind. In real radar applications, such measurements can be very expensive, for example, involving airborne radars with array antennas.In this introductory section we first in Section1.1 define the signal rank and mention some other signal properties. Then in Section 1.2 we present radar applications and other applications where the signal rank is important. Section 1.3 tells what we have done in this article and gives an outline of the rest of the article.


### 1.1. Signal Rank and Other Signal Properties

In many applications of array antennas thecovariance matrixR=E{xxH} of the received signal vector x is utilized. The vector x usually contains the signals from the antenna channels and possibly some temporal dimension. The vector can be called aspace (orspace-only)snapshot orspace-time snapshot, respectively.The rank of the covariance matrix for the case withx containing only external signals and without the white receiver noise is important in radar applications and in many other applications (see Section 1.2). It states how many, in some sense, independent signals impinge on the antenna. We talk about thesignal rank, which is the rank of this covariance matrix.AsR usually is unknown, it must be estimated in the algorithms that use it. A common estimate is [1, 2](1)R^=1NR∑n=1NRxnxnH,where xn are training snapshots and NR is the number of such snapshots. These training snapshots must be selected wisely, depending on the application, and their acquisition will take some time, theacquisition interval. The acquisition of the training data and the estimation of the covariance matrix influence the rank.Other signal properties than the rank which we consider in this article are the DOA (Direction of Arrival) spectrum and eigenpatterns. The DOA spectrum shows the distribution of received power from different DOAs. Eigenpatterns are formed by using the eigenvectors ofR^ as beamforming weights when plotting the antenna array factor. See Section 3.5 for more details.


### 1.2. Applications

Ininterference suppression in radar, the rank of direct and scattered signals is important. Such interference can bedirect path jamming (signals from a jammer travelling one-way line-of-sight to the radar),clutter (signals from the radar transmitter travelling to a surface, where they are undesirably scattered back to the radar, also calledcold clutter), andhot clutter (signals travelling one-way from a jammer to the radar, not directly but scattered on a surface). The received radar signal in a pulse-Doppler radar can be stored in aradar data cube with dimensions for antenna channels (space), pulses (slow-time), and range bins (fast-time). Suppression of interference is commonly performed with linear filters, which can be one-dimensional, two-dimensional, or three-dimensional. For suppression of direct path jamming, space-only snapshots are usually employed, for cold clutter usually space-slow-time and for hot clutter usually space-fast-time.The output of the suppression filter isy=waHx, where x is a received snapshot. The filter weights are usually computed as [3–5](2)wa=μRqq-1w0,where μ is a scalar and Rqq is the covariance matrix of the interference plus (receiver) noise signal vector xq. The vector w0 contains the weights without adaptation. It is usually the steering vector towards the target, possibly with tapering to reduce the sidelobes [5]. The use of filter (2) is commonly calledadaptive beamforming for space-only snapshots or STAP (Space-Time Adaptive Processing) for space-time snapshots (this is also calledoptimal beamforming andoptimal STAP if Rqq is known andadaptive beamforming andadaptive STAP if Rqq is estimated). The interference rank determines the needed DoFs (degrees of freedom = number of filter coefficients minus one) of the filter and the needed number of training snapshots (see, e.g., [4]). The DoF should be at least as many as the rank. There are many proposed methods, calledreduced rank methods, for the suppression, with the DoFs adapted to the rank; for example, see [4, 6, 7].Clutter in bistatic radar (the transmitter and receiver geographically separated) is similar to the case of hot clutter in normal (monostatic) radar. It has been suggested that also bistatic clutter should be suppressed by STAP [8]. Many high resolution DOA, Doppler, and range estimation methods in radar also need to know the signal rank.In applications other than radar, the signal rank is also needed. In Electronic Support Measures (ESM), a kind of electronic warfare, the objective is to learn as much as possible about noncooperative radar and radio transmitters. Among other things, it is desired to estimate the number and location of the transmitters. This information can be used as information only or as a help for jamming. Some methods for estimating the number of emitters and their location need the signal rank. In wireless communication it is suggested to use adaptive beamforming and DOA estimation methods for interuser interference suppression and signal separation [1]. For estimating multipath channel models in wireless communication, DOA estimation can be used [9]. For adaptive beamforming and DOA estimation the signal rank is often needed. In MIMO (Multiple Input Multiple Output) communications, the signal rank is directly related to the transmission capacity.


### 1.3. Description of Work and Outline of Article

This article describes how we have designed and executed low-cost indoor measurements of direct and scattered signals. Direct signals travel one-way in line-of-sight from transmitter antenna to receiver antenna. Scattered signals do not travel in line-of-sight but are scattered on a surface on the way. We have performed the measurements in an anechoic chamber with an experimental array antenna where the received signals arrived directly from the transmitter(s) (direct signals) or were scattered on a moving rough surface reflector (scattered signals). Our experiment takes several aspects into account: transmitted signals with different correlation, decorrelation of the signals during the acquisition interval, covariance matrix estimation, noise eigenvalue spread, calibration, near-field compensation, and scattering on a rough surface. An advantage of indoor measurements in an anechoic chamber compared to outdoor measurements is the good control of the influencing factors, which is necessary to draw objective conclusions.The main result of this paper is the design of the experiment for characterization of signal properties of direct and scattered signals. Also our measured signal properties could be seen as results. They agree with theoretic and simulated results in the literature. We have not seen such measured results but they should exist.In [10], how the space-only rank of direct path signals was dependent on several factors for our experimental array antenna was studied. Also, noise properties were studied. Part of the material in this paper has earlier been published in [11] but the current article contains more details and a significantly deeper analysis.In Section2 we will discuss the relation between rank and eigenvalues and also motivate why we can measure space-time rank with space-only snapshots. Then in Section 3 the experimental setup is described and Section 4 gives some measurement results. A discussion is carried out in Section 5 and, finally, conclusions are presented in Section 6.


## 1.1. Signal Rank and Other Signal Properties

In many applications of array antennas thecovariance matrixR=E{xxH} of the received signal vector x is utilized. The vector x usually contains the signals from the antenna channels and possibly some temporal dimension. The vector can be called aspace (orspace-only)snapshot orspace-time snapshot, respectively.The rank of the covariance matrix for the case withx containing only external signals and without the white receiver noise is important in radar applications and in many other applications (see Section 1.2). It states how many, in some sense, independent signals impinge on the antenna. We talk about thesignal rank, which is the rank of this covariance matrix.AsR usually is unknown, it must be estimated in the algorithms that use it. A common estimate is [1, 2](1)R^=1NR∑n=1NRxnxnH,where xn are training snapshots and NR is the number of such snapshots. These training snapshots must be selected wisely, depending on the application, and their acquisition will take some time, theacquisition interval. The acquisition of the training data and the estimation of the covariance matrix influence the rank.Other signal properties than the rank which we consider in this article are the DOA (Direction of Arrival) spectrum and eigenpatterns. The DOA spectrum shows the distribution of received power from different DOAs. Eigenpatterns are formed by using the eigenvectors ofR^ as beamforming weights when plotting the antenna array factor. See Section 3.5 for more details.


## 1.2. Applications

Ininterference suppression in radar, the rank of direct and scattered signals is important. Such interference can bedirect path jamming (signals from a jammer travelling one-way line-of-sight to the radar),clutter (signals from the radar transmitter travelling to a surface, where they are undesirably scattered back to the radar, also calledcold clutter), andhot clutter (signals travelling one-way from a jammer to the radar, not directly but scattered on a surface). The received radar signal in a pulse-Doppler radar can be stored in aradar data cube with dimensions for antenna channels (space), pulses (slow-time), and range bins (fast-time). Suppression of interference is commonly performed with linear filters, which can be one-dimensional, two-dimensional, or three-dimensional. For suppression of direct path jamming, space-only snapshots are usually employed, for cold clutter usually space-slow-time and for hot clutter usually space-fast-time.The output of the suppression filter isy=waHx, where x is a received snapshot. The filter weights are usually computed as [3–5](2)wa=μRqq-1w0,where μ is a scalar and Rqq is the covariance matrix of the interference plus (receiver) noise signal vector xq. The vector w0 contains the weights without adaptation. It is usually the steering vector towards the target, possibly with tapering to reduce the sidelobes [5]. The use of filter (2) is commonly calledadaptive beamforming for space-only snapshots or STAP (Space-Time Adaptive Processing) for space-time snapshots (this is also calledoptimal beamforming andoptimal STAP if Rqq is known andadaptive beamforming andadaptive STAP if Rqq is estimated). The interference rank determines the needed DoFs (degrees of freedom = number of filter coefficients minus one) of the filter and the needed number of training snapshots (see, e.g., [4]). The DoF should be at least as many as the rank. There are many proposed methods, calledreduced rank methods, for the suppression, with the DoFs adapted to the rank; for example, see [4, 6, 7].Clutter in bistatic radar (the transmitter and receiver geographically separated) is similar to the case of hot clutter in normal (monostatic) radar. It has been suggested that also bistatic clutter should be suppressed by STAP [8]. Many high resolution DOA, Doppler, and range estimation methods in radar also need to know the signal rank.In applications other than radar, the signal rank is also needed. In Electronic Support Measures (ESM), a kind of electronic warfare, the objective is to learn as much as possible about noncooperative radar and radio transmitters. Among other things, it is desired to estimate the number and location of the transmitters. This information can be used as information only or as a help for jamming. Some methods for estimating the number of emitters and their location need the signal rank. In wireless communication it is suggested to use adaptive beamforming and DOA estimation methods for interuser interference suppression and signal separation [1]. For estimating multipath channel models in wireless communication, DOA estimation can be used [9]. For adaptive beamforming and DOA estimation the signal rank is often needed. In MIMO (Multiple Input Multiple Output) communications, the signal rank is directly related to the transmission capacity.


## 1.3. Description of Work and Outline of Article

This article describes how we have designed and executed low-cost indoor measurements of direct and scattered signals. Direct signals travel one-way in line-of-sight from transmitter antenna to receiver antenna. Scattered signals do not travel in line-of-sight but are scattered on a surface on the way. We have performed the measurements in an anechoic chamber with an experimental array antenna where the received signals arrived directly from the transmitter(s) (direct signals) or were scattered on a moving rough surface reflector (scattered signals). Our experiment takes several aspects into account: transmitted signals with different correlation, decorrelation of the signals during the acquisition interval, covariance matrix estimation, noise eigenvalue spread, calibration, near-field compensation, and scattering on a rough surface. An advantage of indoor measurements in an anechoic chamber compared to outdoor measurements is the good control of the influencing factors, which is necessary to draw objective conclusions.The main result of this paper is the design of the experiment for characterization of signal properties of direct and scattered signals. Also our measured signal properties could be seen as results. They agree with theoretic and simulated results in the literature. We have not seen such measured results but they should exist.In [10], how the space-only rank of direct path signals was dependent on several factors for our experimental array antenna was studied. Also, noise properties were studied. Part of the material in this paper has earlier been published in [11] but the current article contains more details and a significantly deeper analysis.In Section2 we will discuss the relation between rank and eigenvalues and also motivate why we can measure space-time rank with space-only snapshots. Then in Section 3 the experimental setup is described and Section 4 gives some measurement results. A discussion is carried out in Section 5 and, finally, conclusions are presented in Section 6.


## 2. Some Preliminaries

What now follows is a discussion of some topics that are needed for and which motivate the article.


### 2.1. Rank and Eigenvalues

The rank of a covariance matrix is equal to the number of eigenvalues larger than zero. However, what matters for interference suppression [4] and number of sources and DOA estimation [1] is the number of eigenvalues larger than the white noise power. This number is called theeffective rank [4]. Theoretically, for a known covariance matrix and for white noise as the only signal, all eigenvalues will be equal and also equal to the noise power. This level is calledthe noise floor. Thus, the effective rank is the number of eigenvalues larger than the noise floor. These eigenvalues are caused by external signals, like targets, clutter, jammers, or radio transmitters and are calledsignal orinterference eigenvalues. The smaller eigenvalues are caused by the receiver noise and are callednoise eigenvalues.In reality the noise eigenvalues will not be equal. There are two reasons. First, the estimated eigenvalues will be different, even if the true covariance matrix has equal eigenvalues, because of estimation errors [4, 10]. If these incorrectly estimated noise eigenvalues are used in the optimal filter (2), the performance will be degraded [4]. Two possible solutions are to set the noise eigenvalues to their correct value (by calibration or appropriate estimation [12]) or to use diagonal loading [4]. When setting the correct noise eigenvalue, the number of signals/interference eigenvalues must be known.The second reason for different noise eigenvalues is that the true eigenvalues really are different due to system nonidealities, like unequal noise power in the channels or correlation between the channels, or due to the used calibration, for example, with a decoupling matrix (Figure1 and Section 3.2). These true unequal noise eigenvalues should not be made equal since the optimal filter (2) needs the true covariance matrix, including true unequal noise eigenvalues.Figure 1
Noise eigenspectrum in measurement C1W (one transmitter and reflector; see Table1). (b) With spatial calibration using a decoupling matrix and (a) without calibration. dB scale. See Section 3.3 for “SM.” See Section 3.5 for an explanation of the figure.
(a) (b)Table 1
Parameters of the measurements.
Name Number of transmitters Correlation PGa Tx 1b [dB] PGa Tx 2b [dB] SNRc [dB] C1S 1 — 0.5 — 41 C2SS 2 Coherent 0.5 - 4.2 45 U2SS 2 Uncorrelated 0.5 - 4.5 40, 32 I2SS 2 Intermediate High High 42 C1W 1 — - 39.5 — 14 C2SW 2 Coherent 0.5 - 44.2 43 U2SW 2 Uncorrelated 0.5 - 44.5 44,-3 aPG is the effective isotropic radiated power[dBm]. bThe DOA was 0° for transmitter 1 (Tx 1) and −15° for transmitter 2 (Tx 2). cThe SNR is for one antenna channel (mean value between the channels) and one time sample after IQ, DDC, and calibration and is estimated from data (by the frequency spectrum, not the Capon spectrum). For measurements C2SS, I2SS, and C2SW the stated SNR is for the sum of the two transmitters. The reason for this is that the transmitters could not be separated in the SNR estimation.To determine the number of signals/interference eigenvalues (of direct and scattered signals) we compute in this article a thresholdλT as the maximum eigenvalue of a measured and estimated noise-only covariance matrix, normalized with the minimum eigenvalue. The threshold then includes the effects due to finite number of snapshots and to nonidealities of the system like unequal and correlated channel noise. The eigenvalues below the threshold are caused by the system (noise and nonidealities) and weak signal/interference eigenvalues. The eigenvalues above the threshold will then, hopefully, only be caused by the external signal/interference sources. Eigenvalues above the threshold will be calledlarge eigenvalues.


### 2.2. Hot Clutter and Space-Only Data

Hot clutter suppression is an important use of our results. Therefore we here explain why our space-only measurements of direct and scattered signals are relevant for hot clutter.The theoretic results in [14] about the estimated space-fast-time hot clutter covariance matrix indicate that the rank of this matrix can be measured by the space-only covariance matrix, if the number of scatterers seen by the receiver is less than the size of the space-only snapshot (which is the case in our measurements since in all experiments the number of large eigenvalues, max 10, is less than the size of the snapshot, 12; see Table 2). Fast-time effects, like jammer and system bandwidth and time-delay to the scatterers, are included in the theoretic model and affect the space-only rank through varying decorrelation of the signals from different scatterers. What determine the rank of space-only or space-fast-time signals are the scatterers and not the number of used samples in space or fast-time. Note that the results in [14] are valid for the estimated covariance matrix (1). This is the covariance matrix that must be used in the signal processing. This is also the one which is used in the analysis of our measurements. With an estimated covariance matrix the acquisition interval, during which decorrelation can occur, is inevitable.Table 2
Summary of eigenspectra resultsa.
Name Figure 1 SM Increase per SMb 12 SMs 24 SMs C1S Figure8 1 1 8 8 C2SS Figure9 1 ≤1 7 8 U2SS Figure10 2 2 (up to 6 SM), ≤1 (above 6 SM) 10 10 I2SS Figure11 2 ≤1 9 10 C1W Figure12 1 0 1 1 C2SW Figure13 1 ≤1 8 8 U2SW Figure14 2 1 8 8 aThe table gives the number of large eigenvalues, that is, eigenvalues larger than the threshold λT. Often the last large eigenvalue came later than the rest. bApproximate values.In [15] the authors measure channel rank in indoor wireless communications by the rank of the time-only covariance matrix of the received signal. They say that in narrowband systems the channel rank is equal to the number of resolvable multipaths for uncorrelated scattering, which with our terminology is the number of uncorrelated sources. This confirms that what determine the rank are the scatterers and not the number of used samples in space or time.


## 2.1. Rank and Eigenvalues

The rank of a covariance matrix is equal to the number of eigenvalues larger than zero. However, what matters for interference suppression [4] and number of sources and DOA estimation [1] is the number of eigenvalues larger than the white noise power. This number is called theeffective rank [4]. Theoretically, for a known covariance matrix and for white noise as the only signal, all eigenvalues will be equal and also equal to the noise power. This level is calledthe noise floor. Thus, the effective rank is the number of eigenvalues larger than the noise floor. These eigenvalues are caused by external signals, like targets, clutter, jammers, or radio transmitters and are calledsignal orinterference eigenvalues. The smaller eigenvalues are caused by the receiver noise and are callednoise eigenvalues.In reality the noise eigenvalues will not be equal. There are two reasons. First, the estimated eigenvalues will be different, even if the true covariance matrix has equal eigenvalues, because of estimation errors [4, 10]. If these incorrectly estimated noise eigenvalues are used in the optimal filter (2), the performance will be degraded [4]. Two possible solutions are to set the noise eigenvalues to their correct value (by calibration or appropriate estimation [12]) or to use diagonal loading [4]. When setting the correct noise eigenvalue, the number of signals/interference eigenvalues must be known.The second reason for different noise eigenvalues is that the true eigenvalues really are different due to system nonidealities, like unequal noise power in the channels or correlation between the channels, or due to the used calibration, for example, with a decoupling matrix (Figure1 and Section 3.2). These true unequal noise eigenvalues should not be made equal since the optimal filter (2) needs the true covariance matrix, including true unequal noise eigenvalues.Figure 1
Noise eigenspectrum in measurement C1W (one transmitter and reflector; see Table1). (b) With spatial calibration using a decoupling matrix and (a) without calibration. dB scale. See Section 3.3 for “SM.” See Section 3.5 for an explanation of the figure.
(a) (b)Table 1
Parameters of the measurements.
Name Number of transmitters Correlation PGa Tx 1b [dB] PGa Tx 2b [dB] SNRc [dB] C1S 1 — 0.5 — 41 C2SS 2 Coherent 0.5 - 4.2 45 U2SS 2 Uncorrelated 0.5 - 4.5 40, 32 I2SS 2 Intermediate High High 42 C1W 1 — - 39.5 — 14 C2SW 2 Coherent 0.5 - 44.2 43 U2SW 2 Uncorrelated 0.5 - 44.5 44,-3 aPG is the effective isotropic radiated power[dBm]. bThe DOA was 0° for transmitter 1 (Tx 1) and −15° for transmitter 2 (Tx 2). cThe SNR is for one antenna channel (mean value between the channels) and one time sample after IQ, DDC, and calibration and is estimated from data (by the frequency spectrum, not the Capon spectrum). For measurements C2SS, I2SS, and C2SW the stated SNR is for the sum of the two transmitters. The reason for this is that the transmitters could not be separated in the SNR estimation.To determine the number of signals/interference eigenvalues (of direct and scattered signals) we compute in this article a thresholdλT as the maximum eigenvalue of a measured and estimated noise-only covariance matrix, normalized with the minimum eigenvalue. The threshold then includes the effects due to finite number of snapshots and to nonidealities of the system like unequal and correlated channel noise. The eigenvalues below the threshold are caused by the system (noise and nonidealities) and weak signal/interference eigenvalues. The eigenvalues above the threshold will then, hopefully, only be caused by the external signal/interference sources. Eigenvalues above the threshold will be calledlarge eigenvalues.


## 2.2. Hot Clutter and Space-Only Data

Hot clutter suppression is an important use of our results. Therefore we here explain why our space-only measurements of direct and scattered signals are relevant for hot clutter.The theoretic results in [14] about the estimated space-fast-time hot clutter covariance matrix indicate that the rank of this matrix can be measured by the space-only covariance matrix, if the number of scatterers seen by the receiver is less than the size of the space-only snapshot (which is the case in our measurements since in all experiments the number of large eigenvalues, max 10, is less than the size of the snapshot, 12; see Table 2). Fast-time effects, like jammer and system bandwidth and time-delay to the scatterers, are included in the theoretic model and affect the space-only rank through varying decorrelation of the signals from different scatterers. What determine the rank of space-only or space-fast-time signals are the scatterers and not the number of used samples in space or fast-time. Note that the results in [14] are valid for the estimated covariance matrix (1). This is the covariance matrix that must be used in the signal processing. This is also the one which is used in the analysis of our measurements. With an estimated covariance matrix the acquisition interval, during which decorrelation can occur, is inevitable.Table 2
Summary of eigenspectra resultsa.
Name Figure 1 SM Increase per SMb 12 SMs 24 SMs C1S Figure8 1 1 8 8 C2SS Figure9 1 ≤1 7 8 U2SS Figure10 2 2 (up to 6 SM), ≤1 (above 6 SM) 10 10 I2SS Figure11 2 ≤1 9 10 C1W Figure12 1 0 1 1 C2SW Figure13 1 ≤1 8 8 U2SW Figure14 2 1 8 8 aThe table gives the number of large eigenvalues, that is, eigenvalues larger than the threshold λT. Often the last large eigenvalue came later than the rest. bApproximate values.In [15] the authors measure channel rank in indoor wireless communications by the rank of the time-only covariance matrix of the received signal. They say that in narrowband systems the channel rank is equal to the number of resolvable multipaths for uncorrelated scattering, which with our terminology is the number of uncorrelated sources. This confirms that what determine the rank are the scatterers and not the number of used samples in space or time.


## 3. Experimental Setup

### 3.1. The Experimental Array Antenna

The experimental receiver antenna [10, 16] used in this article was designed and built by FOI (the Swedish Defence Research Agency). The high quality antenna has sidelobe levels below −60 dB [10, 16] and DOA estimation resolution below one-tenth of the conventional beamwidth [10, 17]. The antenna consists of a horizontal receiving linear array of 12 antenna elements with slightly less than half a wavelength separation (45 mm), 12 receiver modules, 12 A/D converters (12 bits), and 12 buffer memories. The antenna has an agile frequency band of 2.8–3.3 GHz and an instantaneous bandwidth of 5 MHz. The antenna elements are vertically polarized and have a horizontal 3 dB beamwidth of about 115° and a vertical beamwidth of about 15° [10]. The horizontal beamwidth of the whole array is about 10°. The receiver modules were manufactured by Ericsson Microwave Systems (today Saab Electronic Defence Systems). From the buffer memories the signals are transferred to a standard computer, where the IQ-conversion, DDC (digital downconversion and downsampling with a factor of 4), calibration correction, and spatial signal processing are performed in nonreal time. See the hardware block diagrams in [16].The noise properties of our experimental antenna have been investigated by Pettersson in [10]. He stated that the noise sources, without external transmitters, are mainly internal thermal noise from the receiver modules and external thermal noise from the anechoic chamber walls. With external transmitters, there may be additional noise sources, like sampling jitter and phase noise of the signal generators. The true noise power is different in the channels [10] and it may differ by up to 1.5 dB. The noise also has a small correlation between the channels. The absolute value of the nondiagonal elements of the noise covariance matrix can be up to about one-tenth of the diagonal elements [10]. These two noise properties will give spread of the estimated noise eigenvalues; see Section 2.1.


### 3.2. Calibration

Accurate channel equalization (for frequency response) and spatial channel calibration (for mutual coupling) are utilized [10, 16]. The spatial calibration can be performed with three different methods [10](i)
with a DOA correction table on the steering vectors,(ii)
with a decoupling matrix on the steering vectors,(iii)
with a decoupling matrix on the antenna signalsx.The fourth potential method, using a DOA correction table on the antenna signals, is not possible because these signals do not correspond to a single and known DOA. We prefer using a correction table on the steering vectors (method (i)) whenever possible. We have not found any drawbacks with storing such a table instead of only a decoupling matrix, which is contrary to the opinion in [18].If in STAP the spatial calibration is performed on the antenna signalsx (by method (iii)), then the same calibration should be done on the antenna signals xn utilized for the estimation of the interference covariance matrix (1). The reason is to keep the STAP filter (2) optimal, for example, keeping the filter as a matched filter. However, if the spatial calibration is applied on the signals, the internal noise will become more correlated, due to the decoupling matrix [10], and the spread of the noise eigenvalues will be increased (Figure 1 and Section 2.1).Without any spatial calibration the interference suppression performance will be degraded significantly. See Figure2 for an example with a Capon DOA spectrum (Section 3.5) and compare with Figure 10 where spatial calibration is applied (via a DOA correction table on the steering vectors). See also [18]. The Capon spectrum is a form of the STAP filter (2).Figure 2
Capon DOA spectrum without spatial calibration. Otherwise the same measurement (U2SS, two uncorrelated strong transmitters; see Table1) and processing as in Figure 10. See Section 3.5 for an explanation of the figure.


### 3.3. Reflector and Data Acquisition

The measurements were performed in an anechoic chamber at FOI. Both the array antenna and the reflector were horizontally oriented (Figure3). The reflector, made of a fine-meshed aluminum net of size 4.0 m × 1.5 m, was irregularly dented. It was designed to simulate a rough surface with a Gaussian height distribution (with a standard deviation somewhat less than one wavelength) and a Gaussian height correlation function (with a correlation distance of some wavelengths). This surface was chosen to obtain a sufficient number of scattering points from hills and valleys and sufficient roughness to have more than a wavelength bistatic range variation due to the surface roughness. We did not aim to model different terrain types but to achieve multipaths and obtain decorrelation by movement.Figure 3
The reflector and the receiver antenna in the anechoic chamber. Photo from [13].The reflector was suspended from the ceiling using thin ropes at a height which gave grazing angles of about 9°. This grazing angle was just outside of the 3 dB elevation beamwidth (7.5°) of the experimental antenna. This geometry was chosen to have an unobstructed view of the antenna for the direct path signal and to have a sufficient delay corresponding to about one wavelength to obtain a large phase shift for the scattered signals. See Figures4 and 5 for placement of the equipment in the chamber. The suspension allowed the reflector to swing easily from one side to the other.Figure 4
Top view of transmitter and receiver antennas and the reflector in the anechoic chamber. The drawing is not to scale.Figure 5
Side view of transmitter and receiver antennas and the reflector in the anechoic chamber. The drawing is not to scale.When the reflector was swinging back and forth, with a deviation of one to two wavelengths, several submeasurements (SMs) were conducted with a delay of 15 s between the SMs. Each SM contained 256 snapshots (after downconversion and downsampling) and took 40μs to measure. These snapshots were utilized to estimate a covariance matrix (1). The used covariance matrix in the analysis (Section 3.5) is the average of the covariance matrices from the used SMs. The total time for all SMs was about 3 min for 12 SMs (3072 snapshots), 4 min for 16 SMs (4096 snapshots), and 6 min for 24 SMs (6144 snapshots). Increasing the number of used SMs in this study corresponds to increasing the acquisition interval in [14, 19] (denoted as T in [19]). An acquisition interval is needed to estimate the covariance matrix (1).By utilizing several SMs and a swinging reflector we could simulate decorrelation of the direct and scattered signals. The movement of the reflector gave a random component in the phase of the signal. By this the different multipath signals decorrelated with each other and with the direct signal. The movement of the reflector also enabled us to measure an “average” reflector instead of a particular one by using the same reflector at different positions.The use of the reflector was not meant to replicate the exact generation of cold or hot clutter or any other signal/interference. In applications the decorrelation can occur due to movement of transmitter and receiver, nonzero bandwidth, and so forth (see above and Section5).


### 3.4. Transmitters

We used one or two transmitter antennas, which were positioned at about the same height as the receiver antenna. The transmitter antenna 1 was located at the broadside of the receiver antenna and antenna 2 was shifted in DOA (Direction of Arrival) by 15°, which is 1.5 beamwidths of the receiver antenna; see Figure4. Transmitter antenna 1 was a rectangular standard gain horn with a horizontal 3 dB beamwidth of 30°. The second transmitter antenna was a conical ridge horn. The receiver antenna was directed towards transmitter antenna 1, which had DOA 0° seen from the receiver antenna array center.The distance between the transmitter antenna 1 and the receiver antennas was 6.0 m, which is on the limit to be considered a far-field distance for one antenna element. Near-field corrections in the receiver antenna were therefore applied [10, 16]. The far-field (Fraunhofer) region for the receiving antenna is beyond 5 m [20], and the radiating near-field (Fresnel) region is between 0.7 and 5 m. This means that the reflector is in the Fresnel region with almost three times the distance from the reactive near-field. We can therefore assume that there is no coupling between the antenna and the reflector and that the reflector will not influence the receiving antenna properties. By this we conclude that the antenna setup will not influence the decorrelation properties investigated in the article.One or two commercially available signal generators were used for the transmitters. The transmitted waveforms were pure sinusoids, that is, the carrier signal without modulation. Measurements were conducted with coherent, intermediate correlated, and uncorrelated transmitted signals (Figure6). The coherent signals originated from the same signal generator which fed both antennas. The uncorrelated signals were generated by two signal generators with different frequencies. The frequencies were selected so that integer numbers of periods of the sinusoid signal of each transmitter (after downconversion and downsampling) were received during the data acquisition interval. The two transmitted signals then seemed uncorrelated over this interval. This matter is treated in [10]. We believe that the accuracy of the frequencies of the transmitters and the internal oscillators of the receivers was sufficiently good to give sufficiently low correlation between the signals which should be “uncorrelated.” Completely uncorrelated signals are not necessary. Even if the signals are somewhat correlated, the same qualitative behavior is achieved regarding the eigenanalysis [21]. A similar condition for space uncorrelation was noted in [19]. The intermediate correlated signals were generated by two signal generators with the same frequency. The two signal generators were in all cases phase-locked with a 10 MHz signal. The intermediate correlated signals should therefore be close to coherent. The used frequencies for the transmitters were 2999.596875 MHz and 2999.193750 MHz. These frequencies fulfill the requirements described above.Figure 6
Generation of uncorrelated, intermediate correlated, and coherent transmitters. An integral number of periods of the uncorrelated signals fit exactly in the acquisition interval. The frequencyf0 was about 3 GHz and Δf about 0.4 MHz.Table1 lists important measurement parameters of our measurements. The two transmitters were selected to be either nearly equal in strength or very different in strength. This later case could imitate a situation with a weak target signal and a strong jammer. The difference in power, 45 dB, was chosen so that the power of the weak transmitter would be similar to the power of the reflections from the stronger transmitter.


### 3.5. Methods of Reflection Analysis

Our first analysis type employed to describe the direct and scattered signals is theCapon DOA spectrum [22] (also called MVDR, Minimum Variance Distortionless Ratio),(3)Pcaponθ=1aHθR^-1aθ,where a(θ) is the spatial steering vector and R^ is the estimated covariance matrix in (1). The steering vector is a model of how the receiver perceives an impinging signal from direction θ. For us a(θ) was measured in the anechoic chamber and tabulated for -80°≤θ≤80° with a step of 0.5°. For angles θ between the ones in the table the vector aθ was interpolated linearly. The calibration correction for antenna element coupling, amplitude and phase drift, and near-field were all done on the steering vectors. This is method (i) in Section 3.2 (DOA correction table on the steering vectors). See [10, 16] for more information.The Capon spectrum shows the distribution of received power from different DOAs unless the signals are coherent. The Capon spectrum also gives an indication of how well optimal beamforming and STAP can suppress scattered signals, since it is computed according to (2), with special choices of the covariance matrix and the scalar μ. For the Capon spectra, 24 SMs were used. As an example of the influence of the reflector, Figure 7 shows the Capon spectra for experiments with and without the reflector.Figure 7
Capon DOA spectra with the reflector (measurement C1S in Table1, same result as Figure 8) and without the reflector plotted on top of each other. The region between the left and right vertical dashed lines is the reflection region, that is, where reflections are possible because of the presence of the reflector. The middle dashed line(s) is the true DOA of the direct signal(s). 24 SMs.Figure 8
Measurement C1S. A single strong transmitter. (a) Capon DOA spectrum. Figure description in Figure7. (b) Eigenspectrum. Zoom-in to the right. dB scale. See Section 3.3 for “SM.”
(a) (b)The second analysis type is theeigenspectrum, which is the eigenvalues of the antenna signal covariance matrix, usually sorted in decreasing order. We have plotted the eigenvalues in an uncommon manner. They are not plotted in decreasing order for a single covariance matrix but all eigenvalues for the same covariance matrix are plotted in the same “column.” The different columns are used for covariance matrices with different number of SMs. We have computed the eigenvalues for an increasing number of used SMs, up to a maximum of 24. However, in the graphs in this article only up to 16 SMs are plotted, due to space limitations. See Figure 8(b) for an example. The eigenspectrum illustrates the signal/interference rank. In each presentation we have normalized the eigenvalues to the smallest one. No spatial calibration was performed for the eigenspectra results (except as an illustration in Figure 1). For interference suppression this is not necessary, since when computing the optimal weights in (2), the calibration can and should be performed on the quiescent weight vector w0 (method (i) in Section 3.2) instead of the covariance matrix (via a decoupling matrix on the received signals used to estimate the covariance matrix, method (iii)). Done differently, the noise eigenvalue spread would increase (Figure 1) and the noise eigenvectors would influence the optimal filter (2) more and perhaps require more DoFs. In this paper we determine the interference rank by the threshold described in Section 2.1. In the graphs the threshold is marked by the symbol “×”; see Figure 8.We also presenteigenpatterns (eigenvector antenna array factors) [23]. Eigenpatterns are formed by using the eigenvectors of the antenna signal covariance matrix as beamforming weights when plotting the antenna array factor. Since the element pattern is not included in the steering vector, our eigenpatterns will not be antenna patterns. For the eigenpatterns the spatial calibration was performed using a decoupling matrix on the training signals (method (iii) in Section 3.2). See [10, 16] for more information. Since the reflector is not placed in the extreme near-field and the eigenpatterns are transformed to the far-field (by near-field compensation on the training signals and by the used far-field steering vector), there should be no significant differences in the eigenpatterns compared to the case where the reflector is in the far-field.


## 3.1. The Experimental Array Antenna

The experimental receiver antenna [10, 16] used in this article was designed and built by FOI (the Swedish Defence Research Agency). The high quality antenna has sidelobe levels below −60 dB [10, 16] and DOA estimation resolution below one-tenth of the conventional beamwidth [10, 17]. The antenna consists of a horizontal receiving linear array of 12 antenna elements with slightly less than half a wavelength separation (45 mm), 12 receiver modules, 12 A/D converters (12 bits), and 12 buffer memories. The antenna has an agile frequency band of 2.8–3.3 GHz and an instantaneous bandwidth of 5 MHz. The antenna elements are vertically polarized and have a horizontal 3 dB beamwidth of about 115° and a vertical beamwidth of about 15° [10]. The horizontal beamwidth of the whole array is about 10°. The receiver modules were manufactured by Ericsson Microwave Systems (today Saab Electronic Defence Systems). From the buffer memories the signals are transferred to a standard computer, where the IQ-conversion, DDC (digital downconversion and downsampling with a factor of 4), calibration correction, and spatial signal processing are performed in nonreal time. See the hardware block diagrams in [16].The noise properties of our experimental antenna have been investigated by Pettersson in [10]. He stated that the noise sources, without external transmitters, are mainly internal thermal noise from the receiver modules and external thermal noise from the anechoic chamber walls. With external transmitters, there may be additional noise sources, like sampling jitter and phase noise of the signal generators. The true noise power is different in the channels [10] and it may differ by up to 1.5 dB. The noise also has a small correlation between the channels. The absolute value of the nondiagonal elements of the noise covariance matrix can be up to about one-tenth of the diagonal elements [10]. These two noise properties will give spread of the estimated noise eigenvalues; see Section 2.1.


## 3.2. Calibration

Accurate channel equalization (for frequency response) and spatial channel calibration (for mutual coupling) are utilized [10, 16]. The spatial calibration can be performed with three different methods [10](i)
with a DOA correction table on the steering vectors,(ii)
with a decoupling matrix on the steering vectors,(iii)
with a decoupling matrix on the antenna signalsx.The fourth potential method, using a DOA correction table on the antenna signals, is not possible because these signals do not correspond to a single and known DOA. We prefer using a correction table on the steering vectors (method (i)) whenever possible. We have not found any drawbacks with storing such a table instead of only a decoupling matrix, which is contrary to the opinion in [18].If in STAP the spatial calibration is performed on the antenna signalsx (by method (iii)), then the same calibration should be done on the antenna signals xn utilized for the estimation of the interference covariance matrix (1). The reason is to keep the STAP filter (2) optimal, for example, keeping the filter as a matched filter. However, if the spatial calibration is applied on the signals, the internal noise will become more correlated, due to the decoupling matrix [10], and the spread of the noise eigenvalues will be increased (Figure 1 and Section 2.1).Without any spatial calibration the interference suppression performance will be degraded significantly. See Figure2 for an example with a Capon DOA spectrum (Section 3.5) and compare with Figure 10 where spatial calibration is applied (via a DOA correction table on the steering vectors). See also [18]. The Capon spectrum is a form of the STAP filter (2).Figure 2
Capon DOA spectrum without spatial calibration. Otherwise the same measurement (U2SS, two uncorrelated strong transmitters; see Table1) and processing as in Figure 10. See Section 3.5 for an explanation of the figure.


## 3.3. Reflector and Data Acquisition

The measurements were performed in an anechoic chamber at FOI. Both the array antenna and the reflector were horizontally oriented (Figure3). The reflector, made of a fine-meshed aluminum net of size 4.0 m × 1.5 m, was irregularly dented. It was designed to simulate a rough surface with a Gaussian height distribution (with a standard deviation somewhat less than one wavelength) and a Gaussian height correlation function (with a correlation distance of some wavelengths). This surface was chosen to obtain a sufficient number of scattering points from hills and valleys and sufficient roughness to have more than a wavelength bistatic range variation due to the surface roughness. We did not aim to model different terrain types but to achieve multipaths and obtain decorrelation by movement.Figure 3
The reflector and the receiver antenna in the anechoic chamber. Photo from [13].The reflector was suspended from the ceiling using thin ropes at a height which gave grazing angles of about 9°. This grazing angle was just outside of the 3 dB elevation beamwidth (7.5°) of the experimental antenna. This geometry was chosen to have an unobstructed view of the antenna for the direct path signal and to have a sufficient delay corresponding to about one wavelength to obtain a large phase shift for the scattered signals. See Figures4 and 5 for placement of the equipment in the chamber. The suspension allowed the reflector to swing easily from one side to the other.Figure 4
Top view of transmitter and receiver antennas and the reflector in the anechoic chamber. The drawing is not to scale.Figure 5
Side view of transmitter and receiver antennas and the reflector in the anechoic chamber. The drawing is not to scale.When the reflector was swinging back and forth, with a deviation of one to two wavelengths, several submeasurements (SMs) were conducted with a delay of 15 s between the SMs. Each SM contained 256 snapshots (after downconversion and downsampling) and took 40μs to measure. These snapshots were utilized to estimate a covariance matrix (1). The used covariance matrix in the analysis (Section 3.5) is the average of the covariance matrices from the used SMs. The total time for all SMs was about 3 min for 12 SMs (3072 snapshots), 4 min for 16 SMs (4096 snapshots), and 6 min for 24 SMs (6144 snapshots). Increasing the number of used SMs in this study corresponds to increasing the acquisition interval in [14, 19] (denoted as T in [19]). An acquisition interval is needed to estimate the covariance matrix (1).By utilizing several SMs and a swinging reflector we could simulate decorrelation of the direct and scattered signals. The movement of the reflector gave a random component in the phase of the signal. By this the different multipath signals decorrelated with each other and with the direct signal. The movement of the reflector also enabled us to measure an “average” reflector instead of a particular one by using the same reflector at different positions.The use of the reflector was not meant to replicate the exact generation of cold or hot clutter or any other signal/interference. In applications the decorrelation can occur due to movement of transmitter and receiver, nonzero bandwidth, and so forth (see above and Section5).


## 3.4. Transmitters

We used one or two transmitter antennas, which were positioned at about the same height as the receiver antenna. The transmitter antenna 1 was located at the broadside of the receiver antenna and antenna 2 was shifted in DOA (Direction of Arrival) by 15°, which is 1.5 beamwidths of the receiver antenna; see Figure4. Transmitter antenna 1 was a rectangular standard gain horn with a horizontal 3 dB beamwidth of 30°. The second transmitter antenna was a conical ridge horn. The receiver antenna was directed towards transmitter antenna 1, which had DOA 0° seen from the receiver antenna array center.The distance between the transmitter antenna 1 and the receiver antennas was 6.0 m, which is on the limit to be considered a far-field distance for one antenna element. Near-field corrections in the receiver antenna were therefore applied [10, 16]. The far-field (Fraunhofer) region for the receiving antenna is beyond 5 m [20], and the radiating near-field (Fresnel) region is between 0.7 and 5 m. This means that the reflector is in the Fresnel region with almost three times the distance from the reactive near-field. We can therefore assume that there is no coupling between the antenna and the reflector and that the reflector will not influence the receiving antenna properties. By this we conclude that the antenna setup will not influence the decorrelation properties investigated in the article.One or two commercially available signal generators were used for the transmitters. The transmitted waveforms were pure sinusoids, that is, the carrier signal without modulation. Measurements were conducted with coherent, intermediate correlated, and uncorrelated transmitted signals (Figure6). The coherent signals originated from the same signal generator which fed both antennas. The uncorrelated signals were generated by two signal generators with different frequencies. The frequencies were selected so that integer numbers of periods of the sinusoid signal of each transmitter (after downconversion and downsampling) were received during the data acquisition interval. The two transmitted signals then seemed uncorrelated over this interval. This matter is treated in [10]. We believe that the accuracy of the frequencies of the transmitters and the internal oscillators of the receivers was sufficiently good to give sufficiently low correlation between the signals which should be “uncorrelated.” Completely uncorrelated signals are not necessary. Even if the signals are somewhat correlated, the same qualitative behavior is achieved regarding the eigenanalysis [21]. A similar condition for space uncorrelation was noted in [19]. The intermediate correlated signals were generated by two signal generators with the same frequency. The two signal generators were in all cases phase-locked with a 10 MHz signal. The intermediate correlated signals should therefore be close to coherent. The used frequencies for the transmitters were 2999.596875 MHz and 2999.193750 MHz. These frequencies fulfill the requirements described above.Figure 6
Generation of uncorrelated, intermediate correlated, and coherent transmitters. An integral number of periods of the uncorrelated signals fit exactly in the acquisition interval. The frequencyf0 was about 3 GHz and Δf about 0.4 MHz.Table1 lists important measurement parameters of our measurements. The two transmitters were selected to be either nearly equal in strength or very different in strength. This later case could imitate a situation with a weak target signal and a strong jammer. The difference in power, 45 dB, was chosen so that the power of the weak transmitter would be similar to the power of the reflections from the stronger transmitter.


## 3.5. Methods of Reflection Analysis

Our first analysis type employed to describe the direct and scattered signals is theCapon DOA spectrum [22] (also called MVDR, Minimum Variance Distortionless Ratio),(3)Pcaponθ=1aHθR^-1aθ,where a(θ) is the spatial steering vector and R^ is the estimated covariance matrix in (1). The steering vector is a model of how the receiver perceives an impinging signal from direction θ. For us a(θ) was measured in the anechoic chamber and tabulated for -80°≤θ≤80° with a step of 0.5°. For angles θ between the ones in the table the vector aθ was interpolated linearly. The calibration correction for antenna element coupling, amplitude and phase drift, and near-field were all done on the steering vectors. This is method (i) in Section 3.2 (DOA correction table on the steering vectors). See [10, 16] for more information.The Capon spectrum shows the distribution of received power from different DOAs unless the signals are coherent. The Capon spectrum also gives an indication of how well optimal beamforming and STAP can suppress scattered signals, since it is computed according to (2), with special choices of the covariance matrix and the scalar μ. For the Capon spectra, 24 SMs were used. As an example of the influence of the reflector, Figure 7 shows the Capon spectra for experiments with and without the reflector.Figure 7
Capon DOA spectra with the reflector (measurement C1S in Table1, same result as Figure 8) and without the reflector plotted on top of each other. The region between the left and right vertical dashed lines is the reflection region, that is, where reflections are possible because of the presence of the reflector. The middle dashed line(s) is the true DOA of the direct signal(s). 24 SMs.Figure 8
Measurement C1S. A single strong transmitter. (a) Capon DOA spectrum. Figure description in Figure7. (b) Eigenspectrum. Zoom-in to the right. dB scale. See Section 3.3 for “SM.”
(a) (b)The second analysis type is theeigenspectrum, which is the eigenvalues of the antenna signal covariance matrix, usually sorted in decreasing order. We have plotted the eigenvalues in an uncommon manner. They are not plotted in decreasing order for a single covariance matrix but all eigenvalues for the same covariance matrix are plotted in the same “column.” The different columns are used for covariance matrices with different number of SMs. We have computed the eigenvalues for an increasing number of used SMs, up to a maximum of 24. However, in the graphs in this article only up to 16 SMs are plotted, due to space limitations. See Figure 8(b) for an example. The eigenspectrum illustrates the signal/interference rank. In each presentation we have normalized the eigenvalues to the smallest one. No spatial calibration was performed for the eigenspectra results (except as an illustration in Figure 1). For interference suppression this is not necessary, since when computing the optimal weights in (2), the calibration can and should be performed on the quiescent weight vector w0 (method (i) in Section 3.2) instead of the covariance matrix (via a decoupling matrix on the received signals used to estimate the covariance matrix, method (iii)). Done differently, the noise eigenvalue spread would increase (Figure 1) and the noise eigenvectors would influence the optimal filter (2) more and perhaps require more DoFs. In this paper we determine the interference rank by the threshold described in Section 2.1. In the graphs the threshold is marked by the symbol “×”; see Figure 8.We also presenteigenpatterns (eigenvector antenna array factors) [23]. Eigenpatterns are formed by using the eigenvectors of the antenna signal covariance matrix as beamforming weights when plotting the antenna array factor. Since the element pattern is not included in the steering vector, our eigenpatterns will not be antenna patterns. For the eigenpatterns the spatial calibration was performed using a decoupling matrix on the training signals (method (iii) in Section 3.2). See [10, 16] for more information. Since the reflector is not placed in the extreme near-field and the eigenpatterns are transformed to the far-field (by near-field compensation on the training signals and by the used far-field steering vector), there should be no significant differences in the eigenpatterns compared to the case where the reflector is in the far-field.


## 4. Measurement Results

### 4.1. Capon DOA Spectra and Eigenspectra

The Capon DOA spectrum and the eigenspectrum for measurement C1S (a single, strong transmitter; see Table1) are shown in Figure 8. A clear peak at DOA 0° is seen in Figure 8(a). This is the direction of the transmitter. The peak contains both the direct signal and the specular reflection. In the figure the extension of the reflector is given by dashed vertical lines. As seen in the figure, most reflections from the reflector are about 60 dB lower than the peak. We see that the whole reflector is covered by the power from the transmitting antennas. In Figure 8(b), the number of large eigenvalues, that is, above the threshold (Section 2.1), starts with one and increases by one for each new SM, except for the last large eigenvalue, up to a maximum of eight. This means that we can consider the signal/interference rank to be about one to eight, depending on the level of decorrelation, of which the direct signal is one. Table 2 summarizes all eigenspectra.Figure9 presents results from measurement C2SS (two strong coherent transmitters). Here, the Capon spectrum peak for DOA 0° is considerably lower, 30 dB, than in Figure 8. The second direct signal peak is also weak and has some bias in DOA. Most parts of the reflection region are weaker than in Figure 8. The probable reason for the low levels is the mutual cancellation of the signals from the two transmitters due to the coherence between them [21, 24]. The eigenspectrum is similar to Figure 8. This similarity means that two coherent transmitters are seen as a single transmitter. The largest eigenvalue in Figure 9 has nearly the same size as in Figure 8, despite the largest peak being lower in Figure 9 than in Figure 8. This is possible since the eigenvalues do not correspond directly to the power of the signal sources but the sum of the signal eigenvalues λl is equal to the sum of the signal powers Pl [21]:(4)∑l=1LPl=∑l=1Lλl,where L is the number of signal sources.Figure 9
Measurement C2SS. Two coherent strong transmitters. (a) Capon DOA spectrum. (b) Eigenspectrum. Zoom-in to the right. dB scale. See Section3.3 for “SM.”
(a) (b)Figure 10
Measurement U2SS. Two uncorrelated strong transmitters. (a) Capon DOA spectrum. (b) Eigenspectrum. Zoom-in to the right. dB scale. See Section3.3 for “SM.”
(a) (b)The case with two strong uncorrelated transmitters (measurement U2SS) is depicted in Figure10. Both direct signals (including specular reflections) are clearly seen. Also the reflection region is clearly visible. When studying the eigenspectrum, we note a difference to the previous measurements. Here it starts with two large eigenvalues for the first SMs and initially increases by two for each new SM (up to six). Then it increases slower, probably because some eigenvalues are below the noise floor, up to ten large eigenvalues on the remaining SMs.Figure11 shows Capon spectrum and eigenspectrum for the case with two strong and intermediate correlated transmitters (measurement I2SS). The Capon spectrum seems to be nearly identical with the case of uncorrelated transmitters (compare Figures 10 and 11). The eigenspectrum starts with two large eigenvalues and then increases by only one for each extra SM, except for no change between 3 and 4 SMs. The maximum number of large eigenvalues is ten as for uncorrelated transmitters (U2SS) but the final large eigenvalues require more SMs and therefore more decorrelation than for uncorrelated transmitters. The more uncorrelated the transmitters are, the more equal in size the eigenvalues are in the simulations in [19, 21]. In measurement I2SS the transmitters were more correlated than in U2SS. The eigenvalues were probably therefore more unequal and some were too small to cross the threshold and become “large” ones. Thus, the signal/interference rank increases as the correlation between the transmitters decreases.Figure 11
Measurement I2SS. Two intermediate correlated strong transmitters. (a) Capon DOA spectrum. (b) Eigenspectrum. Zoom-in to the right. dB scale. See Section3.3 for “SM.”
(a) (b)In Figure11, we observed that there are two large eigenvalues for a single SM. By changing the analysis to use only 1 SM in 16 repetitions, we obtained two large eigenvalues in 13 repetitions, we obtained one large eigenvalue in 1 repetition, and we obtained three large eigenvalues in 2 repetitions. This shows that with a high probability there will be two large eigenvalues for 1 SM.We now turn to the case with a single weak transmitter (measurement C1W). The Capon spectrum (Figure12) tells us that the peak is 40 dB lower than in Figure 8, which is as expected since the transmitted power was this much lower. The reflection region is not seen at all. The explanation is that the scattered signals are weaker than the noise. The eigenspectrum in Figure 12 contains the same information. It has only one large eigenvalue for all SMs, because of the weak transmitter. All but one eigenvalue are below the noise. See also the discussion about the iceberg effect in Section 5.Figure 12
Measurement C1W. A single weak transmitter. (a) Capon DOA spectrum. (b) Eigenspectrum. Zoom-in to the right. dB scale. See Section3.3 for “SM.”
(a) (b)The Capon DOA spectrum in Figure13 for two coherent and different strong transmitters (measurement C2SW) resembles the one for a single strong transmitter (Figure 8) very much. Also the eigenspectra (Figure 13(b)) are fairly similar for few SMs (compare Figures 8(b) and 13(b)). For up to 6 SMs, the number of large eigenvalues increases by one for each SM as in Figure 8 but the 7th large eigenvalue does not show up until SM 11 for C2SW. The probable reason for the similarity is that the weak transmitter is too weak to disturb the strong transmitter.Figure 13
Measurement C2SW. Two coherent transmitters, one strong and one weak. (a) Capon DOA spectrum. (b) Eigenspectrum. Zoom-in to the right. dB scale. See Section3.3 for “SM.”
(a) (b)In measurement U2SW (two uncorrelated transmitters with different strength) the Capon DOA spectrum (Figure14) is also rather similar to the one with a single strong transmitter (Figure 8). The direct signal is about 3 dB lower and the valleys of the reflection region are deeper. Interestingly, the eigenspectrum (Figure 14) starts with two large eigenvalues, which indicates two noncoherent transmitters despite the low power of the weak transmitter, below the noise (SNR≈-3 dB). This is also possible because of (4). Then the number of large eigenvalues increases by one for each additional SM, which could indicate a single transmitter. It ends with eight large eigenvalues as for a single strong transmitter. There are probably several signal/interference eigenvalues below the noise.Figure 14
Measurement U2SW. Two uncorrelated transmitters, one strong and one weak. (a) Capon DOA spectrum. (b) Eigenspectrum. Zoom-in to the right. dB scale. See Section3.3 for “SM.”
(a) (b)


### 4.2. Eigenpatterns

Figures15 and 16 give some examples of eigenpatterns. More eigenpatterns can be found in [13] according to Table 3. We notice that each eigenpattern has one or more large lobes. When the peak of the highest lobe is within the reflection region (where the reflector can give scattered signals, denoted with the outermost dashed vertical lines), we say that the eigenpatterncovers the reflection region. When the peak is outside this region we say that the eigenpattern covers the region outside.Table 3
Summary of eigenpattern resultsa.
Name 1 SMw ordb 1 SMw/o ordc Figure 12 SMs Figure C1S 8 8 6.8 in [13] 8 6.9 in [13] C2SS 8 8 Figure15 7-8 6.33 in [13] U2SS 5 7 6.24 in [13] 8 6.25 in [13] I2SS 2 6 6.36 in [13] 8 6.37 in [13] C1W 7 7 Figure16 7-8 6.21 in [13] C2SW 5 7 6.16 in [13] 8 6.17 in [13] U2SW 8 8 6.28 in [13] 8 6.29 in [13] aThe table gives the number of eigenpatterns covering the reflection region. b“w ord” stands for “with order” and means the number of covering eigenpatterns in an uninterrupted sequence from the first one. c“w/o ord” means “without order” and means the total number of covering eigenpatterns.Figure 15
Eigenpatterns for measurement C2SS (two coherent strong transmitters). 1 SM. Dashed vertical lines are the true DOAs of the transmitter(s) and the nearest left and right corner of the reflector. Figure6.32 in [13].Figure 16
Eigenpatterns for measurement C1W (a single weak transmitter). 1 SM. Dashed vertical lines are the true DOAs of the transmitter(s) and the nearest left and right corner of the reflector. Figure6.20 in [13].In our measurements the eigenpatterns corresponding to the largest eigenvalues usually cover the reflection region. The remaining eigenpatterns cover the region outside. The one or two largest eigenvalues have eigenpatterns which are directed towards the strong direct signals and the other eigenpatterns usually have nulls in these directions (Figures15 and 16). Actually, the eigenpatterns, associated with the eigenvectors, must be as “different” as possible since they are orthogonal.There is approximately the same number of covering eigenpatterns for 1 SM (“without order”) as for 12 SMs; see Table3.Strangely enough, there is about the same number of eigenpatterns covering the reflection region for 1 SM as there are large eigenvalues using all (24) SMs, especially “without order” (compare Tables2 and 3). Exceptions are the measurement C1W which has 7 covering eigenpatterns (Figure 16) despite only 1 large eigenvalue and U2SS and I2SS, which have somewhat fewer covering eigenpatterns than eigenvalues. C1W seems to observe all distinct sources with its eigenpattern but not with its eigenvalues. Remember some signal eigenvalues are below the noise floor in the eigenspectra.For the weak direct signal in the presence of a strong direct signal, its eigenpattern has a bias in DOA. Also for the case with two equal strong coherent transmitters there is a bias, although less than for two signals with unequal strength.


### 4.3. Summary of the Measurement Results

We have from the measurements obtained results on the rank and other properties of direct and scattered signals. We see that the signal/interference rank depends on the number of transmitters, the SNR (Signal to Noise Ratio), the correlation between the transmitters, and the degree of decorrelation of the transmitter signals that occurs during the data acquisition.Without decorrelation, the direct and scattered signals of a transmitter will all be coherent. If the scattered signals decorrelate with each other and with the direct signal, the rank is increased. Two coherent transmitters appear as a single transmitter regarding the signal/interference rank. Two strong uncorrelated transmitters give rise to the double number of sources compared to a single transmitter.With higher SNR, more eigenvalues of the eigenspectrum tail will appear above the noise level, and the rank will be higher.The eigenpatterns show the reflection region and the DOAs to the direct signals. The eigenpattern can tell us the number of signal sources when the signals still are coherent. Alternatively, they can tell us the extent of the reflection region if the number of signal sources is known.


## 4.1. Capon DOA Spectra and Eigenspectra

The Capon DOA spectrum and the eigenspectrum for measurement C1S (a single, strong transmitter; see Table1) are shown in Figure 8. A clear peak at DOA 0° is seen in Figure 8(a). This is the direction of the transmitter. The peak contains both the direct signal and the specular reflection. In the figure the extension of the reflector is given by dashed vertical lines. As seen in the figure, most reflections from the reflector are about 60 dB lower than the peak. We see that the whole reflector is covered by the power from the transmitting antennas. In Figure 8(b), the number of large eigenvalues, that is, above the threshold (Section 2.1), starts with one and increases by one for each new SM, except for the last large eigenvalue, up to a maximum of eight. This means that we can consider the signal/interference rank to be about one to eight, depending on the level of decorrelation, of which the direct signal is one. Table 2 summarizes all eigenspectra.Figure9 presents results from measurement C2SS (two strong coherent transmitters). Here, the Capon spectrum peak for DOA 0° is considerably lower, 30 dB, than in Figure 8. The second direct signal peak is also weak and has some bias in DOA. Most parts of the reflection region are weaker than in Figure 8. The probable reason for the low levels is the mutual cancellation of the signals from the two transmitters due to the coherence between them [21, 24]. The eigenspectrum is similar to Figure 8. This similarity means that two coherent transmitters are seen as a single transmitter. The largest eigenvalue in Figure 9 has nearly the same size as in Figure 8, despite the largest peak being lower in Figure 9 than in Figure 8. This is possible since the eigenvalues do not correspond directly to the power of the signal sources but the sum of the signal eigenvalues λl is equal to the sum of the signal powers Pl [21]:(4)∑l=1LPl=∑l=1Lλl,where L is the number of signal sources.Figure 9
Measurement C2SS. Two coherent strong transmitters. (a) Capon DOA spectrum. (b) Eigenspectrum. Zoom-in to the right. dB scale. See Section3.3 for “SM.”
(a) (b)Figure 10
Measurement U2SS. Two uncorrelated strong transmitters. (a) Capon DOA spectrum. (b) Eigenspectrum. Zoom-in to the right. dB scale. See Section3.3 for “SM.”
(a) (b)The case with two strong uncorrelated transmitters (measurement U2SS) is depicted in Figure10. Both direct signals (including specular reflections) are clearly seen. Also the reflection region is clearly visible. When studying the eigenspectrum, we note a difference to the previous measurements. Here it starts with two large eigenvalues for the first SMs and initially increases by two for each new SM (up to six). Then it increases slower, probably because some eigenvalues are below the noise floor, up to ten large eigenvalues on the remaining SMs.Figure11 shows Capon spectrum and eigenspectrum for the case with two strong and intermediate correlated transmitters (measurement I2SS). The Capon spectrum seems to be nearly identical with the case of uncorrelated transmitters (compare Figures 10 and 11). The eigenspectrum starts with two large eigenvalues and then increases by only one for each extra SM, except for no change between 3 and 4 SMs. The maximum number of large eigenvalues is ten as for uncorrelated transmitters (U2SS) but the final large eigenvalues require more SMs and therefore more decorrelation than for uncorrelated transmitters. The more uncorrelated the transmitters are, the more equal in size the eigenvalues are in the simulations in [19, 21]. In measurement I2SS the transmitters were more correlated than in U2SS. The eigenvalues were probably therefore more unequal and some were too small to cross the threshold and become “large” ones. Thus, the signal/interference rank increases as the correlation between the transmitters decreases.Figure 11
Measurement I2SS. Two intermediate correlated strong transmitters. (a) Capon DOA spectrum. (b) Eigenspectrum. Zoom-in to the right. dB scale. See Section3.3 for “SM.”
(a) (b)In Figure11, we observed that there are two large eigenvalues for a single SM. By changing the analysis to use only 1 SM in 16 repetitions, we obtained two large eigenvalues in 13 repetitions, we obtained one large eigenvalue in 1 repetition, and we obtained three large eigenvalues in 2 repetitions. This shows that with a high probability there will be two large eigenvalues for 1 SM.We now turn to the case with a single weak transmitter (measurement C1W). The Capon spectrum (Figure12) tells us that the peak is 40 dB lower than in Figure 8, which is as expected since the transmitted power was this much lower. The reflection region is not seen at all. The explanation is that the scattered signals are weaker than the noise. The eigenspectrum in Figure 12 contains the same information. It has only one large eigenvalue for all SMs, because of the weak transmitter. All but one eigenvalue are below the noise. See also the discussion about the iceberg effect in Section 5.Figure 12
Measurement C1W. A single weak transmitter. (a) Capon DOA spectrum. (b) Eigenspectrum. Zoom-in to the right. dB scale. See Section3.3 for “SM.”
(a) (b)The Capon DOA spectrum in Figure13 for two coherent and different strong transmitters (measurement C2SW) resembles the one for a single strong transmitter (Figure 8) very much. Also the eigenspectra (Figure 13(b)) are fairly similar for few SMs (compare Figures 8(b) and 13(b)). For up to 6 SMs, the number of large eigenvalues increases by one for each SM as in Figure 8 but the 7th large eigenvalue does not show up until SM 11 for C2SW. The probable reason for the similarity is that the weak transmitter is too weak to disturb the strong transmitter.Figure 13
Measurement C2SW. Two coherent transmitters, one strong and one weak. (a) Capon DOA spectrum. (b) Eigenspectrum. Zoom-in to the right. dB scale. See Section3.3 for “SM.”
(a) (b)In measurement U2SW (two uncorrelated transmitters with different strength) the Capon DOA spectrum (Figure14) is also rather similar to the one with a single strong transmitter (Figure 8). The direct signal is about 3 dB lower and the valleys of the reflection region are deeper. Interestingly, the eigenspectrum (Figure 14) starts with two large eigenvalues, which indicates two noncoherent transmitters despite the low power of the weak transmitter, below the noise (SNR≈-3 dB). This is also possible because of (4). Then the number of large eigenvalues increases by one for each additional SM, which could indicate a single transmitter. It ends with eight large eigenvalues as for a single strong transmitter. There are probably several signal/interference eigenvalues below the noise.Figure 14
Measurement U2SW. Two uncorrelated transmitters, one strong and one weak. (a) Capon DOA spectrum. (b) Eigenspectrum. Zoom-in to the right. dB scale. See Section3.3 for “SM.”
(a) (b)


## 4.2. Eigenpatterns

Figures15 and 16 give some examples of eigenpatterns. More eigenpatterns can be found in [13] according to Table 3. We notice that each eigenpattern has one or more large lobes. When the peak of the highest lobe is within the reflection region (where the reflector can give scattered signals, denoted with the outermost dashed vertical lines), we say that the eigenpatterncovers the reflection region. When the peak is outside this region we say that the eigenpattern covers the region outside.Table 3
Summary of eigenpattern resultsa.
Name 1 SMw ordb 1 SMw/o ordc Figure 12 SMs Figure C1S 8 8 6.8 in [13] 8 6.9 in [13] C2SS 8 8 Figure15 7-8 6.33 in [13] U2SS 5 7 6.24 in [13] 8 6.25 in [13] I2SS 2 6 6.36 in [13] 8 6.37 in [13] C1W 7 7 Figure16 7-8 6.21 in [13] C2SW 5 7 6.16 in [13] 8 6.17 in [13] U2SW 8 8 6.28 in [13] 8 6.29 in [13] aThe table gives the number of eigenpatterns covering the reflection region. b“w ord” stands for “with order” and means the number of covering eigenpatterns in an uninterrupted sequence from the first one. c“w/o ord” means “without order” and means the total number of covering eigenpatterns.Figure 15
Eigenpatterns for measurement C2SS (two coherent strong transmitters). 1 SM. Dashed vertical lines are the true DOAs of the transmitter(s) and the nearest left and right corner of the reflector. Figure6.32 in [13].Figure 16
Eigenpatterns for measurement C1W (a single weak transmitter). 1 SM. Dashed vertical lines are the true DOAs of the transmitter(s) and the nearest left and right corner of the reflector. Figure6.20 in [13].In our measurements the eigenpatterns corresponding to the largest eigenvalues usually cover the reflection region. The remaining eigenpatterns cover the region outside. The one or two largest eigenvalues have eigenpatterns which are directed towards the strong direct signals and the other eigenpatterns usually have nulls in these directions (Figures15 and 16). Actually, the eigenpatterns, associated with the eigenvectors, must be as “different” as possible since they are orthogonal.There is approximately the same number of covering eigenpatterns for 1 SM (“without order”) as for 12 SMs; see Table3.Strangely enough, there is about the same number of eigenpatterns covering the reflection region for 1 SM as there are large eigenvalues using all (24) SMs, especially “without order” (compare Tables2 and 3). Exceptions are the measurement C1W which has 7 covering eigenpatterns (Figure 16) despite only 1 large eigenvalue and U2SS and I2SS, which have somewhat fewer covering eigenpatterns than eigenvalues. C1W seems to observe all distinct sources with its eigenpattern but not with its eigenvalues. Remember some signal eigenvalues are below the noise floor in the eigenspectra.For the weak direct signal in the presence of a strong direct signal, its eigenpattern has a bias in DOA. Also for the case with two equal strong coherent transmitters there is a bias, although less than for two signals with unequal strength.


## 4.3. Summary of the Measurement Results

We have from the measurements obtained results on the rank and other properties of direct and scattered signals. We see that the signal/interference rank depends on the number of transmitters, the SNR (Signal to Noise Ratio), the correlation between the transmitters, and the degree of decorrelation of the transmitter signals that occurs during the data acquisition.Without decorrelation, the direct and scattered signals of a transmitter will all be coherent. If the scattered signals decorrelate with each other and with the direct signal, the rank is increased. Two coherent transmitters appear as a single transmitter regarding the signal/interference rank. Two strong uncorrelated transmitters give rise to the double number of sources compared to a single transmitter.With higher SNR, more eigenvalues of the eigenspectrum tail will appear above the noise level, and the rank will be higher.The eigenpatterns show the reflection region and the DOAs to the direct signals. The eigenpattern can tell us the number of signal sources when the signals still are coherent. Alternatively, they can tell us the extent of the reflection region if the number of signal sources is known.


## 5. Discussion

### 5.1. Discussion about the Experimental System

To show the eigenvalues for an increasing number of used SMs when the reflector is moving gives the possibility to study the signal/interference rank for different degrees of decorrelation. In a real case, decorrelation can occur as a result of platform motion (comparing with [19]), internal clutter motion, nonzero bandwidth [25], long acquisition interval for estimating the covariance matrix, carrier frequency changes, and so forth.Note that we are studying the estimated covariance matrix (1), not the true covariance matrix. It is the estimated matrix which must be used in algorithms. The measured signal snapshots were space-only snapshots. However, the time dimension enters via the acquisition interval, during which decorrelation of the signals can occur (see also Sections 2.2 and 3.3). This will increase the rank. The decorrelation increases if the acquisition interval is prolonged (more SMs) as in [14].The Capon spectrum gives a good picture of the impinging power from the direct and scattered signals if the transmitters are noncoherent.The measurement result will be influenced by different transmitter signals. With a different frequency of the pure sinusoid, there will be different differences in amplitude and phase between the scatterers on the reflector. If the frequency is changed much, the number of scatters will change and thereby the signal rank will change too, with a higher number and higher rank with a higher frequency. Now the signal bandwidth is low and the scatterers on the reflector cannot be resolved in range (= fast-time). A bandwidth in the order of 100 MHz would be needed to resolve in range. If the transmitter signals are different from pure sinusoids, the emulation of uncorrelated transmitted signals probably had to be performed in a different way.The measurement quality was considered before, during, and after conducting the experiments, for example, with a written experimental design [26] and estimation of uncertainty in the position measurements of the antennas and the reflector. See [13] for further information on this.


### 5.2. More Comparison of the Measurements with the Literature

The literature [19, 21, 27] says that each noncoherent monochromatic source with a different DOA gives rise to a large eigenvalue, which is in accordance with our measurements C1S, C2SS, and U2SS.The more uncorrelated the sources are the more equal in size the eigenvalues are in the experiments in [19, 21]. In particular, uncorrelated sources with well separated DOAs give each an eigenvalue of similar size according to [21]. These statements are in accordance with our measurements I2SS and U2SS. In [25] a theoretic expression for the size of the two eigenvalues of two uncorrelated zero bandwidth signals is derived. In our measurements U2SS and U2SW the difference between the two largest eigenvalues for 1 SM was about 6 dB larger than the prediction of the theory. The discrepancy could be due to a nonideal measurement system and to a nonzero bandwidth because of time limited measurements.The result that the eigenspectrum starts with a single eigenvalue for (one or two) coherent transmitters for a single SM (a very short acquisition interval) in our measurements agrees with the result in [14] showing that the rank will be one for the case without motion and with zero jammer bandwidth and for the case with motion of radar and/or jammer, zero bandwidth, and a “vanishing short” acquisition interval. One of our results is that the number of large eigenvalues will increase up to a limit when the number of SMs is increased. This result is in agreement with the result in [14] showing that each scatterer will appear as an independent source when the acquisition interval goes to infinity.We noticed by our measurements that the number of large eigenvalues depends on the signal power in comparison to the noise floor (compare measurement C1S in Figure8 with C1W in Figure 12 and measurement U2SS with U2SW). The higher the signal power is, the more the eigenvalues of the spectrum tail will appear above the noise level. It is like an iceberg lifting above the ocean surface. This phenomenon is therefore called theiceberg effect. It is described in [4, 27] and there illustrated by simulations.We found that the number of eigenpatterns which cover the reflection region (by the number of eigenpatterns which have their highest peak within the reflection region) is nearly independent of the number of used SMs. To estimate the number of signals using the eigenvalues we need many SMs but with the eigenpatterns it is enough with a few. Thus, it seems like the fact that the eigenpatterns are better for the estimation of the number of signals than the eigenvalues. Nevertheless, it is well-known that the number of large eigenvalues determines the required DoFs for interference suppression [4]. In [27] it is noticed, probably from simulations, that the eigenpatterns corresponding to the signal sources were “essentially unaffected” by a “modest amount” of interference subspace leakage, which is in agreement with our results.We conclude that our measurement results agree in most cases with theoretic and simulated results presented in the literature.


## 5.1. Discussion about the Experimental System

To show the eigenvalues for an increasing number of used SMs when the reflector is moving gives the possibility to study the signal/interference rank for different degrees of decorrelation. In a real case, decorrelation can occur as a result of platform motion (comparing with [19]), internal clutter motion, nonzero bandwidth [25], long acquisition interval for estimating the covariance matrix, carrier frequency changes, and so forth.Note that we are studying the estimated covariance matrix (1), not the true covariance matrix. It is the estimated matrix which must be used in algorithms. The measured signal snapshots were space-only snapshots. However, the time dimension enters via the acquisition interval, during which decorrelation of the signals can occur (see also Sections 2.2 and 3.3). This will increase the rank. The decorrelation increases if the acquisition interval is prolonged (more SMs) as in [14].The Capon spectrum gives a good picture of the impinging power from the direct and scattered signals if the transmitters are noncoherent.The measurement result will be influenced by different transmitter signals. With a different frequency of the pure sinusoid, there will be different differences in amplitude and phase between the scatterers on the reflector. If the frequency is changed much, the number of scatters will change and thereby the signal rank will change too, with a higher number and higher rank with a higher frequency. Now the signal bandwidth is low and the scatterers on the reflector cannot be resolved in range (= fast-time). A bandwidth in the order of 100 MHz would be needed to resolve in range. If the transmitter signals are different from pure sinusoids, the emulation of uncorrelated transmitted signals probably had to be performed in a different way.The measurement quality was considered before, during, and after conducting the experiments, for example, with a written experimental design [26] and estimation of uncertainty in the position measurements of the antennas and the reflector. See [13] for further information on this.


## 5.2. More Comparison of the Measurements with the Literature

The literature [19, 21, 27] says that each noncoherent monochromatic source with a different DOA gives rise to a large eigenvalue, which is in accordance with our measurements C1S, C2SS, and U2SS.The more uncorrelated the sources are the more equal in size the eigenvalues are in the experiments in [19, 21]. In particular, uncorrelated sources with well separated DOAs give each an eigenvalue of similar size according to [21]. These statements are in accordance with our measurements I2SS and U2SS. In [25] a theoretic expression for the size of the two eigenvalues of two uncorrelated zero bandwidth signals is derived. In our measurements U2SS and U2SW the difference between the two largest eigenvalues for 1 SM was about 6 dB larger than the prediction of the theory. The discrepancy could be due to a nonideal measurement system and to a nonzero bandwidth because of time limited measurements.The result that the eigenspectrum starts with a single eigenvalue for (one or two) coherent transmitters for a single SM (a very short acquisition interval) in our measurements agrees with the result in [14] showing that the rank will be one for the case without motion and with zero jammer bandwidth and for the case with motion of radar and/or jammer, zero bandwidth, and a “vanishing short” acquisition interval. One of our results is that the number of large eigenvalues will increase up to a limit when the number of SMs is increased. This result is in agreement with the result in [14] showing that each scatterer will appear as an independent source when the acquisition interval goes to infinity.We noticed by our measurements that the number of large eigenvalues depends on the signal power in comparison to the noise floor (compare measurement C1S in Figure8 with C1W in Figure 12 and measurement U2SS with U2SW). The higher the signal power is, the more the eigenvalues of the spectrum tail will appear above the noise level. It is like an iceberg lifting above the ocean surface. This phenomenon is therefore called theiceberg effect. It is described in [4, 27] and there illustrated by simulations.We found that the number of eigenpatterns which cover the reflection region (by the number of eigenpatterns which have their highest peak within the reflection region) is nearly independent of the number of used SMs. To estimate the number of signals using the eigenvalues we need many SMs but with the eigenpatterns it is enough with a few. Thus, it seems like the fact that the eigenpatterns are better for the estimation of the number of signals than the eigenvalues. Nevertheless, it is well-known that the number of large eigenvalues determines the required DoFs for interference suppression [4]. In [27] it is noticed, probably from simulations, that the eigenpatterns corresponding to the signal sources were “essentially unaffected” by a “modest amount” of interference subspace leakage, which is in agreement with our results.We conclude that our measurement results agree in most cases with theoretic and simulated results presented in the literature.


## 6. Conclusions

We have designed an experiment for low-cost indoor measurements of direct and scattered signals with radar applications in mind. We have good control of the influencing factors, which is necessary to draw objective conclusions. The detailed description of our experiment could serve as a help for conducting other well-controlled experiments. Our experimental design has some characteristics:(i)
Emulation of coherent, intermediate correlated, and uncorrelated signal sources (Section3.4).(ii)
Calibration: when to calibrate and when not and also how to calibrate in different cases (Sections3.2 and 3.5).(iii)
Near-field compensation: relation to receiving antenna properties, decorrelation, and eigenpatterns (Sections3.4 and 3.5).(iv)
Noise eigenvalue spread: relation to calibration, hardware quality, and signal rank (Sections2.1, 3.2, and 3.5).(v)
Emulation of a rough surface by a reflector (Section3.3).(vi)
Decorrelation of the signals by movement of the reflector (Section3.3).(vii)
Acquisition interval for the estimation of the covariance matrix and its effects on the rank (Section3.3).(viii)
Analysis methods: Capon DOA spectrum, eigenspectrum, and eigenpatterns (Section3.5).Section 4.3 summarizes our measured properties of direct and scattered signals. The agreement of our measured properties with theoretic and simulated results presented in the literature shows that our experimental design is realistic and sound.



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