1. Field of the Invention
An aspect of the invention relates to a method for high-resolution imaging of test objects by electromagnetic waves, in particular for inspecting individuals for suspicious items, in which the test object is illuminated with electromagnetic waves, and the scattered waves are received and analyzed using the synthetic aperture radar principle (SAR) to display an image of the test object.
2. Description of the Background Art
In order to inspect individuals or pieces of luggage (hereinafter referred to as test objects) for hidden dangerous items (weapons, explosives), imaging systems are known in which the test objects (individuals, pieces of luggage) are scanned with millimeter waves in order to detect suspicious items (U.S. Pat. No. 5,859,609). The advantage of these imaging systems is that nonmetallic items as well as metallic items can be easily detected due to their material-specific dielectric properties. Similarly, the use of radar-based millimeter wave imaging systems in the field of nondestructive testing of materials (NDT) has increased sharply.
To ensure reliable detection of dangerous items when used in the security field, or of defects in nondestructive testing of materials, the imaging systems require high spatial resolution. Furthermore, it is desirable, especially in applications in the field of security, for the system to be capable of scanning the largest possible area in a short period of time.
High resolution in one plane (lateral resolution) can be achieved with focusing elements, for example elliptical mirrors or dielectric lenses, which sharply focus the measurement signal on the surface of the test object. However, this type of focusing has inadequate depth of focus. High resolution is only provided in one plane, the focal plane. A further disadvantage is that when implementing fast scanning systems using large dielectric lenses or mirrors to concentrate the measurement signals, rapid motion of the large masses can be accomplished mechanically only with difficulty.
German patent application 10 2005 042 463, which is incorporated herein by reference, describes a method of the generic type in which a test object is successively illuminated along its circumference with millimeter waves, and the scattered millimeter waves are received and analyzed using the synthetic aperture radar principle (SAR) to display an image of the test object. A synthetic aperture is created by the means that the waves emitted by an antenna are first spatially concentrated, wherein the location of high concentration is manipulated such that it serves as a moving virtual antenna for SAR analysis.
In this imaging system using the SAR principle, it is known to use no other focusing components for beam forming beyond one antenna (monostatic) or multiple adjacent antennas (quasimonostatic), for example horn antennas, for transmitting and receiving radar signals reflected from the test object. The actual focusing here is performed after the fact by digital signal processing using the SAR principle. This type of data processing permits digital focusing of the raw data for any desired distance of the antenna from the test object. Additional focusing elements such as mirrors or lenses can be omitted, thus drastically reducing the mass of the millimeter wave sensors to be moved.
If a high lateral resolution in two dimensions (vertical and horizontal) is to be achieved with the SAR processing, then the phase center of each transmitting and/or receiving antenna must also be moved in two dimensions. This is achieved in a known manner by a linear motion in the horizontal and vertical direction. The motion of two axes (a raster scan, for example) would be too slow for a fast imaging system.
It is therefore an object of the invention to provide a method for imaging test objects by means of electromagnetic waves that can image as large an area as possible in a short time with high resolution.
This object is achieved in accordance with at least an embodiment of the invention in that the phase centers of the transmitting and receiving antennas can be moved on a circular path parallel to the respective digital focal planes of the imaging system and are substantially simultaneously displaced linearly in another direction parallel to the respective focal plane. The linear displacement here can be in a vertical, horizontal, or inclined direction.
As a result of the rotation of the antenna aperture, which is to say the two-dimensional motion of the antenna phase center, SAR processing of the signals is possible in the vertical and horizontal directions.
Further scope of applicability of the present invention will become apparent from the detailed description given hereinafter. However, it should be understood that the detailed description and specific examples, while indicating preferred embodiments of the invention, are given by way of illustration only, since various changes and modifications within the spirit and scope of the invention will become apparent to those skilled in the art from this detailed description.
The present invention will become more fully understood from the detailed description given hereinbelow and the accompanying drawings which are given by way of illustration only, and thus, are not limitive of the present invention, and wherein:
The imaging systems described below are each part of a test unit used to inspect airline passengers at an airport. The test unit is used to scan airline passengers for suspicious items such as weapons or explosive substances during check-in. The electromagnetic waves used for illuminating the test objects have a frequency between 1 GHz and 10 THz. Preferably, millimeter waves with a frequency between 30 GHz and 300 GHz are used. Either the transmitting antennas themselves, or—as shown in FIGS. 3 through 5—antenna pairs with separate receiving antennas, can be used to receive the reflected waves. Aperture radiators, in particular horn antennas, are preferably used as transmitting and/or receiving antennas.
The test unit can include a platform upon which the test object, for example an airline passenger, is located while the inspection is being carried out. In this process, the transmitting and receiving systems rotate about the stationary test object in order to successively illuminate it along its circumference with millimeter waves. In addition, the test unit includes an analysis system having suitable computing power, which uses the SAR principle to analyze the received waves scattered by the test object in order to obtain an image of the test object. The images produced are displayed to an operator on suitable display devices.
The major parts of the mechanical structure of an inventive imaging system are shown in
It is necessary for SAR processing and for unambiguous interpretation of the measurement results for the transmitting and receiving antennas (antenna pair 1) to each receive the same polarization direction during the rotation. A rotating polarization is possible as well as a permanently fixed polarization direction.
To this end, the antenna pair 1 is rotatably supported in a sleeve with a ball bearing. The sleeve is rigidly connected to a rotary lever 5 that is supported in the device so as to be rotatable about its center point by means of a rotary drive 6. In addition, the antenna pair 1 is connected to the rotary drive 6 of the rotary lever 5 through a combination of two gears 7, 8 and a V-belt 9, wherein a transmission ratio of 1:1 is set, as shown in
The connection between the antennas and the transmitting and receiving unit requires waveguides that have great flexibility, even at high rotational speeds of the antennas. This would only be achievable with enormous technical expenditure using coaxial or hollow waveguide methods, especially for a frequency range above 50 GHz.
Consequently, as shown in
The preferred signal processing is explained in detail below with the aid of
In conventional SAR processing, a spatially invariant correction filter is used. This means that the same correction term is used for reconstructing every pixel. This allows processing with conventional convolution or time-efficient FFT (fast Fourier transform) algorithms.
This spatially invariant correction filter can be used in the case of an imaging geometry with purely Cartesian, polar or spherical coordinates. In the case of the rotating antenna pair 1, which is additionally displaced linearly in a vertical or horizontal direction, as shown in
In contrast to conventional SAR applications, this combined motion requires a few additional processing steps. In an embodiment two different methods of signal processing may be possible according to the invention: an approximated SAR reconstruction in Cartesian coordinates with spatially invariant correction term; or an exact reconstruction in a mixed coordinate system (Cartesian and polar coordinate system) with spatially varying correction term.
The flow diagram of the SAR reconstruction in Cartesian coordinates with spatially invariant correction filter (method 1) is shown in
In order to carry out SAR processing with conventional algorithms from the literature, the measured raw data are first mapped onto a Cartesian coordinate system. This mapping of the raw data is shown in
Due to the mapping of the rotational and linear motion into a Cartesian coordinate system, a new raw data matrix with a nonuniform pixel density results. In order to remedy this, interpolation based on the principle of normalized averaging is then carried out. This is followed by SAR processing with spatially invariant correction filter. This can be carried out by conventional SAR algorithms.
The exact but more time-consuming reconstruction of the raw data is carried out with a spatially varying correction filter in this method. In this process, a separate correction term is required for each pixel. The exact reconstruction of the test object f(x, y, z=Z0) for a distance Z0 between the transmitting and receiving antennas 1 and the test object can be described mathematically as follows. Here, s(x, y, ω) designates the raw data for various angular frequencies ω:
r0: Distance from coordinate origin to the pixel or image point to be reconstructed
rp: Distance from coordinate origin to the surrounding pixels or image points
φ: Angular position on circular path of transmitting/receiving antennas
Δx: Step size of linear motion in horizontal or vertical direction
f(x0,y0,z0,ω)=∫∫s(x,y,ω)ej2k|
{right arrow over (r)}p(x,y,z)=x·{right arrow over (e)}x+y·{right arrow over (e)}y+z·{right arrow over (e)}=
{right arrow over (r)}0(x0,y0,z0)=x0·{right arrow over (e)}x+y0·{right arrow over (e)}y+z0·{right arrow over (e)}=
The integration is replaced by a summation in the real case, since only discrete measurement points are present.
The positions of the transmitting and receiving apertures in Cartesian coordinates can be determined as follows:
Coordinates of the image point to be reconstructed:
x0={tilde over (x)}0+r cos(φ0)
y0=r sin(φ0)
z0=Z0
r: Radius of circular path of the transmitting/receiving aperture
φ0: Angular position on circular path of transmitting/receiving antennas
{tilde over (x)}0: Position in horizontal or vertical direction due to linear motion
Coordinates of the image points:
x={tilde over (x)}+r cos(φ)
y=r sin(φ)
z=0
{tilde over (x)}∈[{tilde over (x)}0−x3dB/2,{tilde over (x)}0+x3dB/2],
φ∈[φ0+φ3dB2,φ0−φ3dB/2]
r: Radius of circular path of the transmitting/receiving aperture
φ: Angular position on circular path of transmitting/receiving antennas
x3dB: Size of the antenna spot in the object plane with reference to the x axis
x3dB=2Z0·a tan(φ3dB/2)
φ3dB: 3 db primary lobe width of the transmitting/receiving aperture
In summary, the phase term φ(x,x0,y,y0,z,z0) of the spatially varying correction filter can be formulated as follows:
Following a pixel-by-pixel reconstruction with the spatially varying correction filter, the data can again be mapped onto a Cartesian coordinate system, and the effect of the nonuniform pixel spacing can again be remedied by the normalized averaging interpolation method.
The invention being thus described, it will be obvious that the same may be varied in many ways. Such variations are not to be regarded as a departure from the spirit and scope of the invention, and all such modifications as would be obvious to one skilled in the art are to be included within the scope of the following claims.
Number | Date | Country | Kind |
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10 2006 006 962 | Feb 2006 | DE | national |
This nonprovisional application is a continuation of International Application No. PCT/EP2006/011630, which was filed on Dec. 5, 2006, and which claims priority to German Patent Application No. 10 2006 006 962.5, which was filed in Germany on Feb. 14, 2006, and which are both herein incorporated by reference.
Number | Name | Date | Kind |
---|---|---|---|
5859609 | Sheen et al. | Jan 1999 | A |
6137437 | Lin et al. | Oct 2000 | A |
7609196 | Jeck et al. | Oct 2009 | B2 |
20030178034 | Yuki | Sep 2003 | A1 |
20080174476 | Detlefsen et al. | Jul 2008 | A1 |
20090051586 | Weinzierl et al. | Feb 2009 | A1 |
Number | Date | Country |
---|---|---|
10 2005 042 463 | Mar 2007 | DE |
2 399 947 | Sep 2004 | GB |
WO 2005050160 | Jun 2005 | WO |
WO 2007093208 | Aug 2007 | WO |
Number | Date | Country | |
---|---|---|---|
20090051586 A1 | Feb 2009 | US |
Number | Date | Country | |
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Parent | PCT/EP2006/011630 | Dec 2006 | US |
Child | 12192096 | US |