CN105629230A - Battlefield vehicle nondestructive detection system and system - Google Patents
Battlefield vehicle nondestructive detection system and system Download PDFInfo
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Abstract
The invention provides a battlefield vehicle nondestructive detection system. The battlefield vehicle nondestructive detection system comprises a transmitting antenna, which is used to transmit millimeter-wave transmitting signals to a battlefield vehicle to be detected; a receiving antenna, which is used to receive echo signals returned by the battlefield vehicle to be detected; a millimeter-wave transceiving module, which is used to generate the millimeter-wave transmitting signals transmitted to the battlefield vehicle to be detected, and is used to receive and process the echo signals from the receiving antenna; a scanning device, which is used to fix and move the millimeter-wave transceiving module, the transmitting antenna, and the receiving antenna; a data acquiring and processing module, which is used for acquiring and processing the echo signals output by the millimeter-wave transceiving module to generate the three-dimensional image of the battlefield vehicle to be detected; and an image display unit, which is used to display the three-dimensional image generated by the data acquiring and processing module. The invention also provides a battlefield vehicle nondestructive detection method adopting the above mentioned battlefield vehicle nondestructive detection system. The structure is simple, and the resolution ratio is high. The imaging time is short, and the visual field is large.
Description
Technical Field
The invention relates to a millimeter wave three-dimensional imaging system based on a linear frequency modulation technology, a superheterodyne detection principle and a holographic imaging principle, in particular to a nondestructive testing system and a nondestructive testing method for a battlefield vehicle.
Background
The frequency of the millimeter wave is 30GHz to 300GHz (the wavelength is from 1mm to 10mm), and in practical engineering application, the low-end frequency of the millimeter wave is usually reduced to 26 GHz. In the electromagnetic spectrum, the position of millimeter wave frequencies lies between the microwave and the infrared. Compared with microwaves, millimeter waves are typically characterized by short wavelength, wide frequency band (having a wide space of use), and propagation characteristics in the atmosphere. Compared with infrared, the millimeter wave has the capability of all-weather work and can be used in severe environments such as smoke, cloud and fog. Under the condition that the microwave frequency band is more and more crowded, the millimeter wave takes the advantages of the microwave into account, and also has some advantages which the low-frequency band microwave does not have.
Specifically, the millimeter wave mainly has the following characteristics: 1. the precision is high, the millimeter wave radar can more easily obtain narrow wave beams and large absolute bandwidth, so that the millimeter wave radar system has stronger anti-electronic interference capability; 2. in the doppler radar, the doppler frequency resolution of the millimeter wave is high; 3. in a millimeter wave imaging system, millimeter waves are sensitive to the shape structure of a target, the capability of distinguishing a metal target from a background environment is strong, and the resolution of the obtained image is high, so that the capability of identifying and detecting the target can be improved by 4, and the millimeter waves can penetrate through plasma; 5. compared with infrared laser, the millimeter wave is less influenced by severe natural environment; 6. the millimeter wave system is small in size and light in weight, so that compared with a microwave circuit, the millimeter wave circuit is much smaller in size, and the millimeter wave system is easier to integrate. It is these unique properties that give millimeter wave technology a wide range of applications, especially in the areas of nondestructive testing and security.
In the initial development stage of millimeter wave imaging, a millimeter wave imaging system uses a single-channel mechanical scanning system, and the imaging system is simple in structure but long in scanning time. To reduce scan time, Millivision corporation developed a Veta125 imager having an 8 x 8 array receive scheme in addition to the transmit scan system, but this imager was more suitable for remote monitoring in large outdoor areas with a field of view of less than 50 cm. Trex corporation has also developed a set of PMC-2 imaging systems in which the antenna elements are implemented using 3mm phased array antenna technology. The PMC-2 imaging system adopts millimeter waves with the center frequency of 84GHz, and the operating frequency of the imaging system is close to the terahertz frequency band, so that the cost is high. LockheedMartin also developed a set of focal plane imaging array imaging systems that used millimeter waves with a center frequency of 94 GHz. TRW developed a passive millimeter wave imaging system that used millimeter waves with a center frequency of 89 GHz. The field of view of the imaging systems of both LockheedMartin and TRW companies is small, typically less than 50 cm.
In the field of millimeter wave imaging, the results of millimeter wave imaging research are mainly focused on the pacific north west laboratory (pacific north western laboratory). Mcmackin et al in this laboratory developed a three-dimensional holographic imaging scanning system whose scanning mechanism was based on cylindrical scanning, and which has achieved commercialization of millimeter wave imaging systems. The imaging system adopts an active imaging mechanism, and obtains a three-dimensional millimeter wave image of a target through inversion of a holographic algorithm. This technology has been licensed from L-3Communications and SaveView Inc. which produce products for use in security inspection systems and try-to-select garments at stations such as stations and docks, respectively. However, because this system uses 384 transceiver units, the cost is never reduced. At present, northwest Pacific laboratories are dedicated to the development and development of millimeter wave imaging systems with higher frequencies.
In addition to the laboratories and companies described above, many scientific research institutes and companies have been involved in the study of millimeter wave imaging technology in countries such as the united kingdom, the united states, such as the army navy air force research laboratory and the navy coastal base, and also in university such as Delaware, Arizona, university such as Reading university in the uk, Durham university, and Farran.
In addition to the united states, the microwave and radar institute (microwaveand radars institute) in germany and the aviation center (germana aeronauticce center) in germany have also participated in the study of millimeter wave imaging technology. The ICT center in Australia, NEC company in Japan, and the like have reports on the results of related millimeter wave imaging studies. However, these units of millimeter wave studies are either in the laboratory phase or the products developed are very expensive or the field of view of detection is small.
The battlefield vehicle used for military purposes is greatly different from a common car, and the military vehicle is often required to adapt to various complicated and severe road conditions and driving conditions in the field, and the harsh environment has high requirements on the performance of the whole vehicle. And the prediction of evaluation indexes such as vehicle fatigue damage deformation is a difficult problem. The traditional solution method has strict requirements on test conditions and consumes a large amount of manpower and material resources. Therefore, the millimeter wave three-dimensional holographic imaging system is adopted to carry out rapid detection, and the efficiency of battlefield vehicle detection can be greatly improved.
Therefore, a millimeter wave three-dimensional imaging detection system with low price and large field of view is needed to realize nondestructive detection of the battlefield vehicle.
Disclosure of Invention
The invention aims to provide a nondestructive testing system for a battlefield vehicle, which has the advantages of simple structure, high resolution and short imaging time.
According to one aspect of the invention, there is provided a nondestructive testing system for a combat vehicle, comprising: the transmitting antenna is used for sending millimeter wave transmitting signals to the tested battlefield vehicle; the receiving antenna is used for receiving an echo signal returned from the tested battlefield vehicle; the millimeter wave transceiver module is used for generating a millimeter wave transmitting signal transmitted to the tested ground vehicle and receiving and processing an echo signal from the receiving antenna; the scanning device is used for fixing and moving the millimeter wave transceiving module, the transmitting antenna and the receiving antenna; the data acquisition and processing module is used for acquiring and processing the echo signals output by the millimeter wave transceiver module to generate a three-dimensional image of the tested battlefield vehicle; and an image display unit for displaying the three-dimensional image generated by the data acquisition and processing module.
Further, the scanning device includes: the two plane detection panels are used for supporting the millimeter wave transceiver module, the transmitting antenna and the receiving antenna, and the tested battlefield vehicle is arranged between the two plane detection panels; the millimeter wave transceiver module, the transmitting antenna and the receiving antenna move up and down along the guide rails; and the motor is used for controlling the up-and-down movement of the millimeter wave transceiving module, the transmitting antenna and the receiving antenna along the guide rail.
Furthermore, each plane detection panel is provided with N millimeter wave transceiver modules, N transmitting antennas and N receiving antennas, each millimeter wave transceiver module corresponds to one transmitting antenna and one receiving antenna, the N millimeter wave transceiver modules are arranged side by side to form a row of millimeter wave transceiver systems, the N transmitting antennas are arranged side by side to form a transmitting antenna array, and the N receiving antennas are arranged side by side to form a receiving antenna array, wherein N is an integer greater than or equal to 2.
Further, the N millimeter wave transceiver modules transmit and receive millimeter waves one by one according to time sequence control.
Further, the millimeter wave transceiver module includes: the transmitting link is used for generating a millimeter wave transmitting signal transmitted to the tested battlefield vehicle; and the receiving link is used for receiving the echo signal returned by the tested battlefield vehicle and processing the echo signal to send to the data acquisition and processing module.
Further, the transmit chain comprises: the first signal source is a frequency modulation signal source working in a first frequency range; the input end of the first directional coupler is connected to a first signal source, and the through end of the first directional coupler is connected to a first power amplifier; the first power amplifier is used for amplifying the power of the output signal of the first directional coupler so as to reach the safe input power range of the first frequency multiplier; and the first frequency multiplier is used for doubling the frequency of the signal output by the first power amplifier to a second frequency range and outputting the doubled signal to the transmitting antenna.
Further, the receiving chain comprises: the second signal source is a dot frequency signal source working at the first frequency; the input end of the first directional coupler is connected to a second signal source; the intermediate frequency end of the first mixer is connected to the through end of the second directional coupler, and the radio frequency end of the first mixer is connected to the coupling end of the first directional coupler so as to generate difference frequency signals of the first signal source and the second signal source; the input end of the second power amplifier is connected to the local oscillator end of the first frequency mixer so as to receive the difference frequency signal, and the power of the difference frequency signal is amplified so as to reach the safe input power range of the second frequency doubler; the input end of the second frequency doubler is connected to the output of the second power amplifier, and the output signal of the second power amplifier is subjected to frequency doubling to a second frequency; the local oscillator end of the second frequency mixer is connected to the output end of the second frequency doubler, and the radio frequency end receives the echo signal received by the receiving antenna to generate a first down-conversion signal; the input end of the third power amplifier is connected to the coupling end of the second directional coupler and is used for carrying out power amplification on the signal from the second directional coupler; the input end of the third frequency doubler is connected to the output end of the third power amplifier, and the second frequency doubler is used for carrying out frequency doubling operation on the signal from the third power amplifier to a second frequency; the local oscillator end of the third mixer is connected to the output end of the third frequency doubler, and the radio frequency end of the third mixer is connected to the intermediate frequency end of the second mixer to generate a secondary down-conversion signal; and the input end of the low-noise amplifier is connected to the intermediate frequency end of the third mixer, amplifies the received secondary down-conversion signal and outputs the amplified secondary down-conversion signal to the data acquisition and processing module.
Further, the first frequency range is 13.5GHz-16.5GHz, the second frequency range is 27GHz-33GHz, the first frequency is 35MHz, and the second frequency is 70 MHz.
Furthermore, in the data acquisition and processing module, echo signals from the millimeter wave transceiver module are acquired, the echo signals are connected with the spatial position signals, and then Fourier transformation and inverse Fourier transformation are carried out to obtain a three-dimensional image.
According to another aspect of the present invention, there is provided a nondestructive testing method for a field vehicle using the nondestructive testing system for a field vehicle, comprising the steps of: the scanning device moves the millimeter wave transceiver module, the transmitting antenna and the receiving antenna to scan the tested battlefield vehicle; the millimeter wave transceiver module generates a millimeter wave transmitting signal; the transmitting antenna transmits the millimeter wave transmitting signal generated by the millimeter wave receiving and transmitting module to the tested battlefield vehicle; the receiving antenna receives an echo signal returned by the tested battlefield vehicle and sends the echo signal to the millimeter wave transceiver module; the millimeter wave transceiver module processes the echo signal and sends the processed echo signal to the data acquisition and processing module; the data acquisition and processing module processes the signals from the millimeter wave transceiver module to generate a three-dimensional image of the tested battlefield vehicle; and an image display unit displays the three-dimensional image generated by the data acquisition and processing module.
Compared with the existing millimeter wave three-dimensional imaging detection system, the technical scheme of the invention simplifies the system structure, improves the resolution, shortens the imaging time and has larger field of view.
Drawings
Fig. 1 is a block diagram of the nondestructive testing system of the battlefield vehicle of the invention.
Fig. 2 is a schematic structural diagram of the nondestructive testing system of the battlefield vehicle.
Fig. 3 is a circuit diagram of a millimeter wave transceiver module in the nondestructive testing system of the battlefield vehicle of the invention.
Fig. 4 is a flow chart of a holographic three-dimensional imaging algorithm performed in the data acquisition and processing module of the nondestructive testing system for a combat vehicle of the present invention.
Fig. 5 is a three-dimensional target imaging schematic diagram of the nondestructive testing system of the battlefield vehicle of the invention.
Fig. 6 is a flow chart of the nondestructive testing method of the battlefield vehicle of the invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
The millimeter wave imaging system is mainly divided into millimeter wave active imaging and millimeter wave passive imaging. The passive millimeter wave imaging system has the advantages of simple structure and low implementation cost, and has the defects of long imaging time and poor imaging resolution. With the improvement of the level of millimeter wave devices and the development of millimeter wave device technology, millimeter wave active imaging is receiving more and more attention. In millimeter wave active imaging, active synthetic aperture imaging and active holographic imaging are the main imaging systems. The millimeter wave holographic imaging method is derived from an optical holographic method, utilizes the coherence principle of electromagnetic waves, firstly a transmitter needs to transmit a high-stability millimeter wave signal, a receiver receives a transmitting signal of each point on a target and performs coherence processing on an echo signal and a highly coherent reference signal, amplitude and phase information of the echo signal is extracted, so that the transmitting characteristic on the target point is obtained, and finally a target millimeter wave image in a scene can be obtained through a data and image processing method. The millimeter wave image obtained by the millimeter wave active holographic imaging has good resolution, can greatly shorten the imaging time when being matched with mechanical scanning, and can realize engineering, so the millimeter wave active holographic imaging is particularly suitable for millimeter wave short-range active imaging.
Embodiments of the present invention are described in detail below with reference to the accompanying drawings.
Fig. 1 is a block diagram of the nondestructive testing system of the battlefield vehicle of the invention. Fig. 2 is a schematic structural diagram of the nondestructive testing system of the battlefield vehicle.
As shown in FIG. 1, the nondestructive testing system for the battlefield vehicle of the invention comprises: the transmitting antenna 14 is used for sending millimeter wave transmitting signals to the tested battlefield vehicle; a receiving antenna 15 for receiving the echo signal returned from the tested battlefield vehicle; the millimeter wave transceiver module 11 is used for generating a millimeter wave transmitting signal sent to the tested ground vehicle and receiving and processing an echo signal from the receiving antenna 15; a scanning device 10 for fixing and moving the millimeter wave transceiver module 11, the transmitting antenna 14, and the receiving antenna 15; the data acquisition and processing module 12 is used for acquiring and processing the echo signals output from the millimeter wave transceiver module 11 to generate a three-dimensional image of the tested battlefield vehicle; and an image display unit 13 for displaying the three-dimensional image generated by the data acquisition and processing module 12.
As shown in fig. 2, the scanning device 10 is composed of a vertical direction guide 21, a motor (e.g., a stepping motor) 22, and a plane detection panel 23. Specifically, the scanning device 10 includes two plane detection panels 23 for supporting the millimeter wave transceiver module 11, the transmitting antenna 14, and the receiving antenna 15, and the measured chariot 24 is disposed between the two plane detection panels 23. The scanning device 10 further includes two pairs of guide rails 21 respectively disposed on both sides of each plane detection panel 23, and the millimeter wave transceiver module 11, the transmitting antenna 14, and the receiving antenna 15 move up and down along the guide rails 21. The scanning device 10 further comprises a control motor 22 located beside the detection panel 23, and is used for controlling the up-and-down movement of the millimeter wave transceiver module 11, the transmitting antenna 14 and the receiving antenna 15 along the guide rail 21, so as to scan the tested battlefield vehicle 24 up and down.
As further shown in fig. 2, N millimeter wave transceiver modules 11, N transmitting antennas 14, and N receiving antennas 15 are disposed on each plane detection panel 23, each millimeter wave transceiver module 11 corresponds to one transmitting antenna 14 and one receiving antenna 15, the N millimeter wave transceiver modules 11 are disposed side by side to form a row of millimeter wave transceiver systems, the N transmitting antennas 14 are disposed side by side to form a transmitting antenna array, and the N receiving antennas 15 are disposed side by side to form a receiving antenna array, where N is an integer greater than or equal to 2.
In addition, the N millimeter wave transceiver modules 11 are controlled according to the time sequence to transmit and receive millimeter waves one by one, so that the horizontal scanning of the tested battlefield vehicle is completed. For example, the control of the N millimeter wave transceiver modules 11 may be implemented by a single-pole multi-throw switch, but any timing control device known in the art may be used.
In addition, the tested battlefield vehicle can also move to improve the imaging speed.
It should be further noted that the number of the millimeter wave transceiver modules 11 and the corresponding transmitting antennas 14 and receiving antennas 15 included in the millimeter wave transceiver system in a row may be set according to the width of the plane detection panel 23 and the imaging speed to be achieved, and the width of the plane detection panel 23 may be determined according to the size of the tested field vehicle 24. In addition, the distance between the plane detection panel 23 and the measured battlefield vehicle 24 can be determined according to the antenna parameters and other indexes. The arrangement of the above mentioned dimensions is obvious for a person skilled in the art and will therefore not be described in detail.
For example, the row 1 millimeter wave transceiver system may include 64 millimeter wave transceiver modules 11 and 128 antennas, wherein 1-64 transmitting antennas constitute the transmitting antenna array 14 for radiating the chirped continuous wave generated by the 64 millimeter wave transceiver modules 11 onto the target 24 to be measured, and 65-128 receiving antennas constitute the receiving antenna array 15 for receiving the signal reflected by the battlefield vehicle to be measured and transmitting the signal to the 64 millimeter wave transceiver modules 11. Each transmit antenna corresponds to a receive antenna, and transmit antennas 1, 2, 3, …, 63, and 64 correspond to receive antennas 65, 66, 67, …, 127, and 128, respectively. As described above, the 64 millimeter wave transceiver modules 11 do not operate simultaneously, but are controlled by, for example, two layers of single-pole multi-throw switches, so that they transmit and receive one by one,
fig. 3 is a circuit diagram of a millimeter wave transceiver module in the nondestructive testing system of the battlefield vehicle of the invention.
As shown in fig. 3, the millimeter wave transceiver module 11 includes: the transmitting link consists of a signal source 301, a directional coupler 302, a power amplifier 303 and a frequency doubler 304 and is used for generating a millimeter wave transmitting signal sent to the tested battlefield vehicle 24; and a receiving link, which is composed of a signal source 307, a directional coupler 309, mixers 310, 312, 313, power amplifiers 311, 314, frequency doublers 312, 315 and a low noise amplifier 317, and is used for receiving the echo signals returned by the tested battlefield vehicle 24 and processing the echo signals to send to the data acquisition and processing module 12.
Specifically, the signal source 301 is a frequency modulation signal source with an operating frequency in a certain frequency range (e.g., 13.5GHz-16.5GHz), and can be expressed as:
where A1 is expressed as the initial amplitude, f1The initial scanning frequency is 13.5GHz, t is time,is the initial phase value of the signal source 301, B is the bandwidth of the frequency modulated signal, and T is the frequency modulated period.
Furthermore, the signal source 307 is a single frequency continuous wave signal source with an operating frequency at a fixed frequency (e.g., 35MHz), and can be expressed as:
with initial amplitude and phase a2 andthe frequency is f 2.
Note that the frequency range of the signal source 301 and the frequency of the signal source 307 may be selected according to resolution requirements and the like, which are well known to those skilled in the art and will not be described herein.
The directional coupler 302 is a three-port device, the input end of which receives the output signal of the signal source 301, and the through end of which is connected to the power amplifier 303, so that the power of the transmission link reaches the safe input power range of the frequency doubler 304. After passing through the frequency doubler 304, the frequency of the transmission link is doubled to a second frequency range (in the case of the signal source 301 having a frequency range of 13.5GHz-16.5GHz, the frequency range here is 27GHz-33GHz), and finally radiated by a transmission antenna into the space to reach the tested battlefield vehicle. Here, the transmission signal may be expressed as:
wherein A is1' is the amplitude of the transmitted signal.
The output signal of the second signal source 307 is connected to the input of the directional coupler 309. The mixer 310 is a three-port device, in which the IF terminal of the intermediate frequency is connected to the through terminal of the directional coupler 309 to input an intermediate frequency signal of, for example, 35MHz, the RF terminal of the radio frequency is connected to the coupling terminal of the directional coupler 302 to input a frequency modulated signal of, for example, 13.5GHz to 16.5GHz, and the LO terminal of the local oscillator outputs a difference frequency signal between the signals input from the RF and IF terminals to the power amplifier 311. The power amplifier 311 amplifies the signal power to within the safe operating range of the frequency doubler 312. At this time, the output signal of the frequency doubler 312 is a signal obtained by mixing two signal sources and then doubling the frequency, which can be expressed as:
the mixer 313 is a three-port device, wherein the LO terminal is connected to the output signal s (t) of the frequency doubler 312, and the RF terminal obtains the echo signal reflected from the measured battlefield vehicle received by the receiving antenna 15. The echo signal at this time can be expressed as:
where α is an echo signal attenuation coefficient, τ ═ 2R/c is an echo delay generated by the object to be measured, and c is a propagation speed of the electromagnetic wave in space.
The intermediate frequency IF end of the mixer 313 outputs a superheterodyne signal of the local oscillator LO and the signal received by the radio frequency RF end, where the signal has certain spatial target information, which may be represented as:
the non-coherence of the two signal sources can be seen from equation (6), and a mixer 316 is introduced to obtain a coherent signal. The mixer 316 outputs a coherent superheterodyne signal with target information, and the radio frequency end thereof inputs the first down-converted signal S from the mixer 313IF(t), the local oscillator inputs the continuous wave signal of, for example, 70MHz output by the signal source 307 through the coupling terminal of the directional coupler 309, the power amplifier 314 and the frequency doubler 315, that is:
wherein A is2' is the signal amplitude.
The intermediate frequency IF terminal of the mixer 316 outputs a second down-converted signal S with target informationIF(t), namely:
as can be seen from equation (8), the phase asynchronism introduced by the incoherent dual signal source is eliminated by this method.
The low noise amplifier 317 can amplify the weak intermediate frequency signal after two down conversions, so as to improve the signal-to-noise ratio and the detection sensitivity of the output signal, and the output signal is sent to the data acquisition and processing module 12.
Fig. 4 is a flow chart of a holographic three-dimensional imaging algorithm performed in the data acquisition and processing module of the nondestructive testing system for a combat vehicle of the present invention.
As shown in fig. 4, the data acquisition and processing module 12 first acquires echo information from the acquired signals (401), and associates the acquired echo information with the spatial location signals. And then, Fourier transform (402) of geometric characteristics is carried out by utilizing Fourier transform, Fourier inverse transform (403) is carried out after simplification and deformation, a target three-dimensional image (404) is finally obtained, and the final data is obtained by combining the spatial domain position information.
Fig. 5 is a three-dimensional target imaging schematic diagram of the nondestructive testing system of the battlefield vehicle of the invention.
As shown in fig. 5, after the millimeter wave passes through the scattering at the position point (X, Y, Z) of the target 502, the receiving antenna 501 at the position (X, Y, Z0) starts receiving the scattered broadband echo signal. The antenna sends the received signal to the millimeter wave circuit and the highly coherent local oscillator signal for down conversion, and then to the low noise amplifier 317. Let the resulting signal be E (X, Y, ω), where ω is the instantaneous angular frequency of the emission source, and E (X, Y, ω) is a function of ω, expressed as:
wherein,is the distance between the antenna and the target point,the index part represents spherical wave signals scattered by the target and plays an important role in three-dimensional scattering imaging of the target. And:
e (X, Y, ω) is a time domain signal, which is an expression of fourier transform of the time dimension signal E (X, Y, t), that is:
E(X,Y,ω)＝FT[E(X,Y,t)](11)
the expression (10) is taken into the expression (9), the vector operation of the expression (9) is simplified into the scalar operation, and it can be understood from the physical sense that a spherical wave is expanded and expressed as the superposition of plane waves to obtain:
the three-dimensional fourier transform is used in equation (12), namely:
also an inverse fourier transform, namely:
by omitting the constant term in equation (13), substituting equation (13) into equation (12) yields:
and (3) performing inverse transformation on the formula (15) to obtain a final broadband millimeter wave holographic imaging formula:
as can be seen from equation (16), as long as the electromagnetic information of the echo signal of each frequency point is obtained, f (x, y, z) can be obtained through a series of inversions, and finally, the three-dimensional millimeter wave holographic image of the imaging target is obtained.
Fig. 6 is a flow chart of the nondestructive testing method of the battlefield vehicle of the invention.
As shown in fig. 6, the millimeter wave holographic three-dimensional imaging detection method for the tested war chariot by using the nondestructive detection system for the war chariot comprises the following steps: the scanning device moves the millimeter wave transceiver module, the transmitting antenna and the receiving antenna to scan the tested battlefield vehicle; the millimeter wave transceiver module generates a millimeter wave transmitting signal; the transmitting antenna transmits the millimeter wave transmitting signal generated by the millimeter wave receiving and transmitting module to the tested battlefield vehicle; the receiving antenna receives an echo signal returned by the tested battlefield vehicle and sends the echo signal to the millimeter wave transceiver module; the millimeter wave transceiver module processes the echo signal and sends the processed echo signal to the data acquisition and processing module; the data acquisition and processing module processes the signals from the millimeter wave transceiver module to generate a three-dimensional image of the tested battlefield vehicle; and an image display unit displays the three-dimensional image generated by the data acquisition and processing module.
Compared with the existing millimeter wave imaging instrument, the nondestructive detection system and method for the battlefield vehicle have the following outstanding advantages that:
(1) the price is low: the invention uses the driving motor to realize the scanning effect of the area array of the one-dimensional array antenna, thereby greatly reducing the cost.
(2) Simple structure, easy integration: the invention adopts a single-pole multi-throw switch and the like to control the working sequence of the channel of the millimeter wave transceiver module, and adopts a frequency modulation signal source and a millimeter wave device to build a system, thereby greatly reducing the complexity of the system and simultaneously improving the integration level of the system.
(3) The resolution is high: the invention adopts frequency modulation continuous wave technology, super heterodyne technology and holographic imaging technology, and improves the resolution of three-dimensional image plane and depth.
(4) The imaging time is fast: the invention adopts the motor to drive the transmitting-receiving antenna to move up and down, and simultaneously can lead the tested battlefield vehicle to move forward at a certain speed, thereby greatly improving the imaging speed.
(5) The field of view is increased: compared with the existing field of view below 50 cm, the embodiment of the invention can reach the field of view of several meters or even dozens of meters.
(6) The signal-to-noise ratio is high: the system adopts active millimeter wave imaging, improves the transmitting power of the antenna by controlling the output power range of each millimeter wave device, certainly, the transmitting power is in the safe radiation range, so that the signal-to-noise ratio of echo signals is far higher than that of signals received by a passive millimeter wave imaging system, and further higher imaging quality is obtained.
(7) The application is wide: by utilizing the advantages of high resolution, simple structure and the like of the millimeter wave imaging technology, the nondestructive detection of the battlefield vehicle can be carried out, the damage of the outer layer of various large-scale instruments can be detected, and the method is also suitable for the detection of contraband.
It should be noted that the above-mentioned embodiments described with reference to the drawings are only intended to illustrate the present invention and not to limit the scope of the present invention, and it should be understood by those skilled in the art that modifications and equivalent substitutions can be made without departing from the spirit and scope of the present invention. Furthermore, unless the context indicates otherwise, words that appear in the singular include the plural and vice versa. Additionally, all or a portion of any embodiment may be utilized with all or a portion of any other embodiment, unless stated otherwise.
Claims (10)
1. A nondestructive inspection system for a combat tank, said security inspection system comprising:
the transmitting antenna is used for sending millimeter wave transmitting signals to the tested battlefield vehicle;
the receiving antenna is used for receiving an echo signal returned from the tested battlefield vehicle;
the millimeter wave transceiver module is used for generating a millimeter wave transmitting signal sent to the tested ground war vehicle and receiving and processing the echo signal from the receiving antenna;
the scanning device is used for fixing and moving the millimeter wave transceiving module, the transmitting antenna and the receiving antenna;
the data acquisition and processing module is used for acquiring and processing the echo signals output by the millimeter wave transceiver module to generate a three-dimensional image of the tested battlefield vehicle; and
an image display unit for displaying the three-dimensional image generated by the data acquisition and processing module.
2. The nondestructive testing system for a combat vehicle of claim 1 wherein said scanning device comprises:
the two plane detection panels are used for supporting the millimeter wave transceiver module, the transmitting antenna and the receiving antenna, and the to-be-tested battlefield vehicle is arranged between the two plane detection panels;
the millimeter wave transceiver module, the transmitting antenna and the receiving antenna move up and down along the guide rails; and
and the motor is used for controlling the millimeter wave transceiver module, the transmitting antenna and the receiving antenna to move up and down along the guide rail.
3. The nondestructive inspection system for battle field vehicles according to claim 2, wherein N millimeter wave transceiver modules, N transmitting antennas and N receiving antennas are provided on each plane inspection panel, each millimeter wave transceiver module corresponding to one transmitting antenna and one receiving antenna, the N millimeter wave transceiver modules are arranged side by side to form a row of millimeter wave transceiver systems, the N transmitting antennas are arranged side by side to form a transmitting antenna array, and the N receiving antennas are arranged side by side to form a receiving antenna array, where N is an integer greater than or equal to 2.
4. The nondestructive testing system for a battlefield vehicle as claimed in claim 3, wherein said N millimeter wave transceiver modules transmit and receive millimeter waves one by one according to timing control.
5. The nondestructive testing system for a combat vehicle of claim 1 wherein said millimeter wave transceiver module comprises:
the transmitting link is used for generating a millimeter wave transmitting signal which is sent to the tested battlefield vehicle; and
and the receiving link is used for receiving the echo signal returned by the tested battlefield vehicle and processing the echo signal so as to send the echo signal to the data acquisition and processing module.
6. The nondestructive testing system for a combat vehicle of claim 5 wherein said transmit chain comprises:
a first signal source, the first signal source being a frequency modulated signal source operating in a first frequency range;
the input end of the first directional coupler is connected to the first signal source, and the through end of the first directional coupler is connected to the first power amplifier;
the first power amplifier amplifies the power of the output signal of the first directional coupler to reach the safe input power range of the first frequency multiplier; and
the first frequency multiplier doubles the frequency of the signal output by the first power amplifier to a second frequency range, and outputs the doubled frequency signal to the transmitting antenna.
7. The nondestructive testing system for a combat vehicle of claim 6 wherein said receiving link comprises:
a second signal source, the second signal source being a dot frequency signal source operating at a first frequency;
a second directional coupler, an input end of the first directional coupler being connected to the second signal source;
a first mixer, wherein an intermediate frequency end of the first mixer is connected to a through end of the second directional coupler, and a radio frequency end of the first mixer is connected to a coupling end of the first directional coupler, so as to generate difference frequency signals of the first signal source and the second signal source;
the input end of the second power amplifier is connected to the local oscillator end of the first frequency mixer so as to receive the difference frequency signal, and the power of the difference frequency signal is amplified so as to reach the safe input power range of a second frequency doubler;
the input end of the second frequency doubler is connected to the output of the second power amplifier, and the output signal of the second power amplifier is subjected to frequency doubling to a second frequency;
a local oscillator end of the second mixer is connected to an output end of the second frequency doubler, and a radio frequency end receives the echo signal received by the receiving antenna to generate a first down-conversion signal;
the input end of the third power amplifier is connected to the coupling end of the second directional coupler and is used for carrying out power amplification on the signal from the second directional coupler;
a third frequency doubler, an input end of which is connected to an output end of the third power amplifier, and which doubles the frequency of the signal from the third power amplifier to the second frequency;
a local oscillator end of the third mixer is connected to the output end of the third frequency doubler, and a radio frequency end of the third mixer is connected to the intermediate frequency end of the second mixer to generate a secondary down-conversion signal; and
and the input end of the low-noise amplifier is connected to the intermediate frequency end of the third mixer, amplifies the received secondary down-conversion signal and outputs the amplified secondary down-conversion signal to the data acquisition and processing module.
8. The nondestructive testing system for a combat vehicle of claim 7 wherein said first frequency range is 13.5GHz-16.5GHz, said second frequency range is 27GHz-33GHz, said first frequency is 35MHz, and said second frequency is 70 MHz.
9. The nondestructive testing system of claim 1 wherein said data acquisition and processing module acquires echo signals from said millimeter wave transceiver module, associates the echo signals with spatial location signals, and then performs fourier and inverse fourier transforms to obtain three-dimensional images.
10. A method of nondestructive testing of a field vehicle using the nondestructive testing system of any one of claims 1 to 9, comprising the steps of:
the scanning device moves the millimeter wave transceiver module, the transmitting antenna and the receiving antenna to scan the tested battlefield vehicle;
the millimeter wave transceiver module generates a millimeter wave transmitting signal;
the transmitting antenna transmits the millimeter wave transmitting signal generated by the millimeter wave transceiver module to the tested battlefield vehicle;
the receiving antenna receives an echo signal returned by the tested battlefield vehicle and sends the echo signal to the millimeter wave transceiver module;
the millimeter wave transceiver module processes the echo signal and sends the echo signal to the data acquisition and processing module;
the data acquisition and processing module processes signals from the millimeter wave transceiver module to generate a three-dimensional image of the tested battlefield vehicle; and
the image display unit displays the three-dimensional image generated by the data acquisition and processing module.
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