CN111965614B - Maneuvering weak target detection method based on dynamic programming and minimum image entropy - Google Patents

Maneuvering weak target detection method based on dynamic programming and minimum image entropy Download PDF

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CN111965614B
CN111965614B CN202010730392.2A CN202010730392A CN111965614B CN 111965614 B CN111965614 B CN 111965614B CN 202010730392 A CN202010730392 A CN 202010730392A CN 111965614 B CN111965614 B CN 111965614B
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CN111965614A (en
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胡程
王锐
蔡炯
龙腾
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Beijing Institute of Technology BIT
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/41Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00 using analysis of echo signal for target characterisation; Target signature; Target cross-section
    • G01S7/415Identification of targets based on measurements of movement associated with the target
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/41Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00 using analysis of echo signal for target characterisation; Target signature; Target cross-section
    • G01S7/418Theoretical aspects

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Abstract

The invention provides a maneuvering weak target detection method based on dynamic programming and minimum image entropy, which comprises the steps of firstly, rapidly searching the most probable movement track of a weak target, namely the movement track with the maximum echo energy by using a dynamic programming method; then extracting a target signal, performing FFT to obtain a frequency spectrum of the target signal, taking the image entropy as a cost function, utilizing a Newton method to iterate and quickly search high-order components of the target so as to minimize the image entropy of the frequency spectrum, finally utilizing CA-CFAR to determine a threshold, comparing the maximum value of the compensated frequency spectrum with a detection threshold to judge whether the target exists or not, and providing an effective means for maneuvering weak target detection in radar; therefore, the method uses the DP technology to search the possible track of the target, has higher running speed, can correct the range migration caused by the maneuvering of the target, realizes the coherent accumulation of signals, has high running speed, can compensate the motion component of any order, and has higher detection efficiency and accuracy in the aspect of maneuvering weak target detection in the radar.

Description

Maneuvering weak target detection method based on dynamic programming and minimum image entropy
Technical Field
The invention belongs to the technical field of radar detection, and particularly relates to a maneuvering weak target detection method based on Dynamic Programming (DP) and Minimum Image Entropy (MIE).
Background
Long-term coherent accumulation methods are often used to detect weak targets. However, in the accumulation process, the target may be mobile, which causes range migration and doppler frequency migration, so that the energy of a weak target is difficult to be effectively accumulated and detected.
In the conventional coherent accumulation method, the Keystone transform is a common method for resolving the range migration of a target. The basic principle of Keystone transformation is to decouple the Doppler frequency of a target echo signal from time delay through slow time scale transformation, so as to eliminate the influence of range migration. However, the Keystone transform is only suitable for eliminating range migration in case of uniform motion. When the target is maneuvering, Keystone transformation can only eliminate partial range migration amount caused by initial velocity, and cannot eliminate range migration caused by high-order motion component of the target. In addition, the Keystone transform has the defects of large calculation amount, fuzzy target speed needing to be estimated in advance and the like.
For Doppler frequency migration caused by maneuvering, a coherent accumulation method for performing high-order phase compensation by using Fractional Fourier transform (FrFT) and generalized Radon-Fourier transform (GRFT) is provided. FrFT is an extension of the conventional fourier transform to compensate for higher order phases by converting the signal to the fractional frequency domain to remove the effects of the second order phase. However, FrFT can only compensate for phase changes caused by acceleration, and cannot do so for jerks and higher order motion components. GRFT is similar to an exhaustive method, which realizes coherent accumulation by jointly searching motion component parameters such as velocity, acceleration, jerk, etc., and it can compensate phase change caused by any high-order component, but it involves joint search of multiple parameters, and often cannot be accepted in terms of computation.
Therefore, for radar maneuvering weak target detection, a coherent accumulation detection algorithm capable of efficiently compensating for high-order motion of a target is urgently needed.
Disclosure of Invention
In order to solve the problems, the invention provides a maneuvering weak target detection method based on dynamic programming and minimum image entropy.
A maneuvering weak target detection method based on dynamic programming and minimum image entropy comprises the following steps:
s1: receiving K frames of radar echo signals, and acquiring a track of a weak target with the largest echo energy from the K frames of radar echo signals by adopting a dynamic programming method, wherein each frame of radar echo signals corresponds to one frame of one-dimensional range profile, the one-dimensional range profile comprises a plurality of range units, and the track is formed by the range units where the weak target is located in each frame of one-dimensional range profile;
s2: extracting each of weak targetsEcho data corresponding to each distance unit, and then constructing a track echo signal s corresponding to a weak target according to the extracted echo signals DP (k):
Figure BDA0002603004160000021
Wherein A is r For a set target amplitude, λ is the radar wavelength, T is the pulse repetition period of the radar, a 1 ~a H H is a undetermined coefficient, H is 1,2, …, H is a set order, j is an imaginary part, K is 1,2, …, K;
s3: for the track echo signal s DP (k) Performing phase compensation and fourier transform to obtain a compensated spectrum s (m):
Figure BDA0002603004160000031
wherein m is a frequency point,
Figure BDA0002603004160000032
is a phase compensation amount, and
Figure BDA0002603004160000033
s4: obtaining the image entropy E of the spectrum s (m):
Figure BDA0002603004160000034
wherein C is a set constant;
s5: the following objective function is constructed according to the image entropy E:
Figure BDA0002603004160000035
wherein a ═ a 2 ,...,a h ,...,a H ];
S6: let a 1 After being equal to 0, then adoptResolving the target function by using a Newton method to obtain a undetermined coefficient a 1 ~a H To obtain the final frequency spectrum S end (m);
S7: obtaining a spectrum S end (m) peak value S end (m 0 ) Wherein m is 0 Is the peak value S end (m 0 ) The frequency point of the position;
s8: determine | S end (m 0 )| 2 Whether the threshold value is less than the set CA-CFAR threshold value V T If the target is smaller than the target, the weak target is a false alarm target, and if the target is not smaller than the target, the weak target is a real target.
Further, the method for acquiring the track of the weak target with the maximum echo energy from the K-frame radar echo signals by using the dynamic programming method comprises the following steps:
s11: initial value of the set-point function
Figure BDA0002603004160000036
Figure BDA0002603004160000037
Wherein,
Figure BDA0002603004160000038
the state of the nth range cell in the one-dimensional range profile corresponding to the 1 st frame of radar echo signal is shown, and the state comprises a target and no target,
Figure BDA0002603004160000039
the square of the amplitude of the radar echo signal of the nth range unit in the one-dimensional range profile corresponding to the 1 st frame of radar echo signal is obtained;
s12: according to the initial value of the value function corresponding to each distance unit in the 1 st stage, iterative calculation is carried out by adopting the following formula to obtain the value function corresponding to each distance unit from the 2 nd stage to the K th stage
Figure BDA0002603004160000041
Wherein each stage isAcquiring a frame of radar echo signals:
Figure BDA0002603004160000042
Figure BDA0002603004160000043
wherein,
Figure BDA0002603004160000044
and the state of the nth range unit in the one-dimensional range profile corresponding to the kth frame of radar echo signal is defined, the state comprises a target and no target, K is 1,2, …, K,
Figure BDA0002603004160000045
is the square of the amplitude of the radar echo signal for the nth range bin,
Figure BDA0002603004160000046
is the most probable transition to the state in all the states of the k-1 stage
Figure BDA0002603004160000047
A state of (A) and
Figure BDA0002603004160000048
for all possible transitions to state in the k-1 stage
Figure BDA0002603004160000049
Max is a function of the maximum value, arg denotes that
Figure BDA00026030041600000410
Taking the corresponding state at the time of maximum value as
Figure BDA00026030041600000411
S13: recording the state corresponding to the maximum value of the value function obtained in the K stage as
Figure BDA00026030041600000412
Wherein n is 0 Is in a state
Figure BDA00026030041600000413
The serial number of the located distance unit;
s14: based on the state of the K stage
Figure BDA00026030041600000414
Obtaining the most probable transition to State in stage K-1
Figure BDA00026030041600000415
State of (1)
Figure BDA00026030041600000416
Then, the most possible transition state to the K-2 stage is obtained
Figure BDA00026030041600000417
State of (1)
Figure BDA00026030041600000418
And repeating the steps until the 1 st stage is reached, and obtaining the track of the weak target with the maximum echo energy.
Further, the setting method of the setting constant C is as follows:
Figure BDA00026030041600000419
further, the CA-CFAR threshold V T The setting method comprises the following steps:
Figure BDA00026030041600000420
wherein, P fa In order to set the false alarm rate, R is 1,2, …, R is the number of reference frequency points, S end (m r ) Is a reference frequency point m r Of spectral values of, whereinThe method for acquiring the reference frequency point comprises the following steps:
at frequency point m 0 Taking the frequency points with the set number on the left and right sides as protection frequency points;
the protection frequency points at the outermost peripheries of the left side and the right side are respectively taken as starting points and extend to the left side and the right side, and the frequency points with set quantity on the left side and the right side are taken as reference frequency points.
Further, the target function is solved by adopting a Newton method to obtain an undetermined coefficient a 1 ~a H The value of (b) specifically comprises the following steps:
s61: let a be [ a ] 2 ,...,a h ,...,a H ]Is 0, the initial value of the image entropy E is obtained, then the coefficient updating operation is executed on the initial value of the image entropy E, and the updated undetermined coefficient a is obtained 2 ~a H (ii) a Wherein the coefficient updating operation specifically comprises:
s61 a: respectively with a 2 ~a H Obtaining the entropy E of the image to be determined as a variable 2 ~a H First partial derivative of
Figure BDA0002603004160000051
Figure BDA0002603004160000052
Figure BDA0002603004160000053
Wherein, Imag represents an imaginary part, and represents conjugation;
s61 b: treating a fixed coefficient a based on image entropy E 2 ~a H First partial derivative of
Figure BDA0002603004160000054
Then obtaining the image entropy E to-be-determined coefficient a 2 ~a H Second partial derivative of
Figure BDA0002603004160000055
Figure BDA0002603004160000056
Wherein,
Figure BDA0002603004160000057
and l represents the amount of phase compensation in the second partial derivative
Figure BDA0002603004160000061
The serial number of (2);
s61 c: calculating the cross term in the second partial derivative according to whether k and l are equal
Figure BDA0002603004160000062
Wherein when k is l:
Figure BDA0002603004160000063
wherein, Re represents a real part, and IDFT represents inverse discrete Fourier transform;
when k ≠ l:
Figure BDA0002603004160000064
s61 d: the first partial derivative
Figure BDA0002603004160000065
And second partial derivative
Figure BDA0002603004160000066
Are respectively marked as
Figure BDA0002603004160000067
And
Figure BDA0002603004160000068
then according to
Figure BDA0002603004160000069
And
Figure BDA00026030041600000610
updating the undetermined coefficient a 2 ~a H
Figure BDA00026030041600000611
Wherein,
Figure BDA00026030041600000612
is a coefficient to be determined h The iteration value obtained in the (i + 1) th iteration,
Figure BDA00026030041600000613
is a coefficient to be determined h The iteration value obtained in the ith iteration, I is the iteration number, and I is 0,1,2, …, I and I are the set upper limit value of the iteration number,
Figure BDA00026030041600000614
is a ═ a 2 ,...,a h ,...,a H ]0;
s62: judging the updated undetermined coefficient a 2 ~a H Whether the iteration termination condition is reached or not, if any iteration termination condition is met, the undetermined coefficient a obtained by the iteration is obtained 2 ~a H If the values are not satisfied, the step S63 is entered, where the iteration termination condition is:
each undetermined coefficient a 2 ~a H Corresponding first derivative
Figure BDA0002603004160000071
The absolute values of the difference values with 0 are all smaller than a set threshold value;
the iteration times reach an iteration time upper limit value I;
s63: adopting the updated undetermined coefficient a 2 ~a H The entropy E of the image is updated, thenRe-executing the coefficient updating operation on the updated image entropy E to obtain a secondary updated undetermined coefficient a 2 ~a H (ii) a And so on until the updated undetermined coefficient a 2 ~a H An iteration end condition is reached.
Has the beneficial effects that:
the invention provides a maneuvering weak target detection method based on dynamic programming and minimum image entropy, which comprises the steps of firstly, quickly searching a weak target most likely, namely a movement track with maximum echo energy by using a dynamic programming method; then extracting a target signal, performing FFT to obtain a frequency spectrum of the target signal, taking the image entropy as a cost function, utilizing a Newton method to iterate and quickly search high-order components of the target so as to minimize the image entropy of the frequency spectrum, finally utilizing CA-CFAR to determine a threshold, comparing the maximum value of the compensated frequency spectrum with a detection threshold to judge whether the target exists or not, and providing an effective means for maneuvering weak target detection in radar; compared with the existing distance migration correction methods such as Keystone conversion and the like, the method has the advantages that the possible track of the target is searched by using the DP technology, the running speed is higher, and the distance migration caused by target maneuvering can be corrected; compared with the existing phase compensation methods such as FrFT and GRFT, the method disclosed by the invention has the advantages that the target high-order motion component is quickly searched in an iterative manner by minimizing the image entropy of the signal frequency spectrum, the coherent accumulation of the signal is realized, the running speed is high, and the motion component of any order can be compensated; in conclusion, the invention has higher detection efficiency and accuracy in the aspect of maneuvering weak target detection in the radar.
Drawings
FIG. 1 is a flow chart of a method for detecting a maneuvering weak target based on dynamic programming and minimum image entropy according to the present invention;
FIG. 2 is a schematic distance-time plane of a radar echo provided by the present invention;
FIG. 3 is a diagram of an initial spectrum provided by the present invention;
FIG. 4 is a diagram illustrating iteration of high-order motion components provided by the present invention using Newton's method;
FIG. 5 is a diagram of a DP-MIE processed spectrum according to the present invention.
Detailed Description
In order to make the technical solutions better understood by those skilled in the art, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application.
As shown in FIG. 1, the invention provides a coherent accumulation detection algorithm combining dynamic programming and minimum image entropy, which first searches a possible target track and corrects range migration by using a dynamic programming algorithm; then extracting a track echo and performing FFT (fast Fourier transform) to obtain a frequency spectrum of the track echo, and carrying out fast iterative search on high-order motion components such as acceleration and jerk by a Newton method to minimize the image entropy of the frequency spectrum by taking the image entropy as a cost function; and finally, compensating a high-order phase of the target signal by using the searched high-order motion parameters to finish coherent accumulation, and setting a threshold by using a Cell-average constant false alarm (CA-CFAR) detection method to finish the detection of the weak target. The overall process comprises the following steps:
s1: receiving K frames of radar echo signals, and acquiring a track of a weak target with the largest echo energy from the K frames of radar echo signals by adopting a dynamic programming method, wherein each frame of radar echo signal corresponds to one frame of one-dimensional range profile, the one-dimensional range profile comprises a plurality of range units, and the track is formed by the range units of the weak target in each frame of one-dimensional range profile.
It should be noted that the dynamic programming method searches for a track by energy recursion of the echo signal on the distance-time plane, and can quickly screen out a track with higher energy, which is used as a possible track of a target. The specific implementation steps of the DP technology for quickly searching the possible target track are as follows:
s11: initial value of the set-point function
Figure BDA0002603004160000091
Figure BDA0002603004160000092
Wherein,
Figure BDA0002603004160000093
the state of the nth range unit in the one-dimensional range profile corresponding to the 1 st frame of radar echo signal is obtained, the state comprises a target and no target,
Figure BDA0002603004160000094
the square of the amplitude of the radar echo signal of the nth range unit in the one-dimensional range profile corresponding to the 1 st frame of radar echo signal is obtained;
s12: according to the initial value of the value function corresponding to each distance unit in the 1 st stage, iterative calculation is carried out by adopting the following formula to obtain the value function corresponding to each distance unit from the 2 nd stage to the K th stage
Figure BDA0002603004160000095
To achieve accumulation of a value function, wherein each stage acquires a frame of radar echo signals:
Figure BDA0002603004160000096
Figure BDA0002603004160000097
wherein,
Figure BDA0002603004160000098
also known as a cost function or cumulative observation, which records the state of the kth stage along a certain trajectory (this trajectory is
Figure BDA0002603004160000099
) A non-coherent accumulation of the observed values of (a);
Figure BDA00026030041600000910
the state of the nth range unit in the one-dimensional range profile corresponding to the kth frame radar echo signal is shown, the state comprises a target and no target, and K is 1,2, …, K;
Figure BDA00026030041600000911
the square of the amplitude of the radar echo signal for the nth range bin also represents the pair state
Figure BDA00026030041600000912
The observed value of (a);
Figure BDA00026030041600000913
is the most probable transition to the state in all the states of the k-1 stage
Figure BDA00026030041600000914
And is set to 0 at initialization, i.e.
Figure BDA00026030041600000915
For representing the starting point of the track;
Figure BDA00026030041600000916
for all possible transitions to state in the k-1 stage
Figure BDA00026030041600000917
Max is a function of the maximum value, arg denotes that
Figure BDA00026030041600000918
Taking the corresponding state at the maximum value as
Figure BDA00026030041600000919
S13: recording the state corresponding to the maximum value of the value function obtained in the K stage as
Figure BDA00026030041600000920
Wherein n is 0 Is in a state
Figure BDA00026030041600000921
The number of the located distance unit.
It should be noted that this step is to screen the value function, and in the K stageFinding the maximum value function and obtaining the corresponding state of the value function
Figure BDA0002603004160000101
As shown in the following formula:
Figure BDA0002603004160000102
s14: based on the state of the K stage
Figure BDA0002603004160000103
Obtaining the most probable transition to State in stage K-1
Figure BDA0002603004160000104
State of (1)
Figure BDA0002603004160000105
Then, the most possible transition to the state in the K-2 stage is obtained
Figure BDA0002603004160000106
State of (1)
Figure BDA0002603004160000107
And repeating the steps until the 1 st stage is reached, and obtaining the track of the weak target with the maximum echo energy, namely the maximum sum of the value functions.
Further, the process of backtracking is formulated as follows:
Figure BDA0002603004160000108
wherein track (k) indicates that the final state is
Figure BDA0002603004160000109
State of the trace in the k-th stage.
S2: extracting echo data corresponding to each distance unit where the weak target is located, and then constructing the weak target according to the extracted echo signalsCorresponding track echo signal s DP (k):
Figure BDA00026030041600001010
Wherein, A r For a set target amplitude, λ is the radar wavelength, T is the pulse repetition period of the radar, a 1 ~a H To be a coefficient of undetermination, a h And a motion component representing the H-th order of the target, wherein the first order is velocity, the second order is acceleration, the third order is jerk, and the like, H is 1,2, …, H is a set order, j is an imaginary part, and K is 1,2, …, K.
S3: for the track echo signal s DP (k) Performing phase compensation and fourier transform to obtain compensated spectrum s (m):
Figure BDA00026030041600001011
wherein, m is a frequency point,
Figure BDA0002603004160000111
is a phase compensation quantity, and
Figure BDA0002603004160000112
that is, after the dynamic programming process, range migration of weak targets has been corrected and the target signal s extracted DP (k) If phase compensation is needed, the compensated spectrum s (m) can be obtained by FFT.
S4: obtaining the image entropy E of the spectrum s (m):
Figure BDA0002603004160000113
wherein C is a set constant equal to the total energy of the signal sequence, and
Figure BDA0002603004160000114
it should be noted that the image entropy may represent the confusion and complexity of the image. The larger the entropy, the more chaotic (defocused), random, complex the image; conversely, the smaller the image entropy, the more ordered (focused), regular, and simple the image. When the entropy value reaches the theoretical minimum value of 0, the image energy is completely focused at one point. In radar data processing, if target signal Doppler migration compensation is not performed, when a target has a high-order motion component, MTD processing is directly performed on a target echo signal, the energy of the target is divergent on a frequency spectrum (the entropy value is large), and the target cannot be ideally focused on a certain frequency. This results in a reduction in pulse accumulation gain, which is detrimental to subsequent target detection. If MTD processing is performed after the compensation of the higher-order motion component is completed, a good focused spectrum (with a small entropy value) can be obtained. Therefore, the image entropy is used as a cost function, and then high-order motion components such as acceleration and jerk are quickly and iteratively searched through a Newton method so as to minimize the image entropy of the frequency spectrum; then, compensating the high-order phase of the target signal by using the searched high-order motion parameters to complete phase-coherent accumulation, and setting a threshold by using a CA-CFAR detection method to complete the detection of the weak target, specifically referring to steps S5-S8:
s5: the following objective function is constructed according to the image entropy E:
Figure BDA0002603004160000115
wherein a ═ a 2 ,...,a h ,...,a H ]。
It should be noted that when
Figure BDA0002603004160000121
Satisfy the requirements of
Figure BDA0002603004160000122
The image entropy E of the spectrum is minimal, so that the higher order motion component a is a cost function of the image entropy E 2 ,...,a h ,...,a H Optimizing the entropy E of the frequency spectrum image for the variable needing to be optimizedAnd obtaining the target function.
S6: let a 1 When the value is equal to 0, then the objective function is solved by adopting Newton method to obtain undetermined coefficient a 1 ~a H To obtain the final frequency spectrum S end (m), comprising the steps of:
s61: let a be [ a ] 2 ,...,a h ,...,a H ]Is 0, the initial value of the image entropy E is obtained, then the coefficient updating operation is executed on the initial value of the image entropy E, and the updated undetermined coefficient a is obtained 2 ~a H (ii) a Wherein the coefficient updating operation specifically comprises:
s61 a: respectively with a 2 ~a H Obtaining the entropy E of the image to be determined as a variable 2 ~a H First partial derivative of
Figure BDA0002603004160000123
Figure BDA0002603004160000124
Figure BDA0002603004160000125
Wherein, Imag represents an imaginary part, and one represents conjugation;
s61 b: treating a fixed coefficient a based on image entropy E 2 ~a H First partial derivative of
Figure BDA0002603004160000126
Then obtaining the image entropy E to-be-determined coefficient a 2 ~a H Second partial derivative of
Figure BDA0002603004160000127
Figure BDA0002603004160000128
Wherein,
Figure BDA0002603004160000129
and l represents the amount of phase compensation in the second partial derivative
Figure BDA0002603004160000131
The serial number of (2);
s61 c: calculating the cross term in the second partial derivative according to whether k and l are equal
Figure BDA0002603004160000132
Wherein, when k ═ l:
Figure BDA0002603004160000133
wherein Re represents a real part, and IDFT represents inverse discrete Fourier transform;
when k ≠ l:
Figure BDA0002603004160000134
s61 d: first partial derivative of
Figure BDA0002603004160000135
And second partial derivative
Figure BDA0002603004160000136
Are respectively marked as
Figure BDA0002603004160000137
And with
Figure BDA0002603004160000138
Then according to
Figure BDA0002603004160000139
And
Figure BDA00026030041600001310
updating the undetermined coefficient a 2 ~a H
Figure BDA00026030041600001311
Wherein,
Figure BDA00026030041600001312
is a coefficient to be determined h The iteration value obtained in the (i + 1) th iteration,
Figure BDA00026030041600001313
is a coefficient to be determined h The iteration value obtained in the ith iteration, I is the iteration number, and I is 0,1,2, …, I is the set upper limit value of the iteration number,
Figure BDA00026030041600001314
is a ═ a 2 ,...,a h ,...,a H ]0;
s62: judging the updated undetermined coefficient a 2 ~a H Whether the iteration termination condition is met or not, if any iteration termination condition is met, the undetermined coefficient a obtained by the iteration is obtained 2 ~a H If the values are not satisfied, the step S63 is entered, where the iteration termination condition is:
each coefficient to be determined a 2 ~a H Corresponding first derivative
Figure BDA0002603004160000141
The absolute values of the difference values with 0 are all smaller than a set threshold value;
the iteration times reach an iteration time upper limit value I;
s63: adopting the updated undetermined coefficient a 2 ~a H Updating the image entropy E, and then re-executing coefficient updating operation on the updated image entropy E to obtain a secondary updated undetermined coefficient a 2 ~a H (ii) a And so on until the updated undetermined coefficient a 2 ~a H An iteration end condition is reached.
S7: obtaining a spectrum S end (m) peak value S end (m 0 ) Wherein m is 0 Is the peak value S end (m 0 ) The frequency point of the position;
s8: judging | S end (m 0 )| 2 Whether is less than the set CA-CFAR threshold V T If the weak target is smaller than the target, the weak target is a false alarm target, and if the weak target is not smaller than the target, the weak target is a real target.
The CA-CFAR threshold V T The setting method comprises the following steps:
Figure BDA0002603004160000142
wherein, P fa In order to set the false alarm rate, R is 1,2, …, R is the number of reference frequency points, S end (m r ) Is a reference frequency point m r The reference frequency point is obtained by the following steps:
at frequency point m 0 Taking the frequency points with the set number on the left and right sides as protection frequency points;
the protection frequency points at the outermost peripheries of the left side and the right side are respectively taken as starting points and extend to the left side and the right side, and the frequency points with set quantity on the left side and the right side are taken as reference frequency points.
To verify the validity of the accumulation detection method described previously. The method is based on simulation experiment data, and the maneuvering weak target detection algorithm combining dynamic programming and minimum image entropy is adopted to complete the detection of the maneuvering weak target. The parameters of the simulation are shown in table 1:
TABLE 1 simulation parameters
Parameter(s) Value of
Radar wavelength 0.02m
Center frequency of radar 16GHz
Bandwidth of radar 800MHz
Pulse repetition frequency 500Hz
Width of distance unit 0.12m
Target motion component [ a 1 ,a 2 ,a 3 ] [0.8,0.3,0.1]
Target signal-to-noise ratio 3dB
The range-time plane of the radar echo is shown in fig. 2, which has 500 pulses of radar echo data, the target begins to appear at 540m, and significant maneuvers occur during the movement.
Step one, DP finds the target track:
and performing modular calculation on the multi-frame one-dimensional range profile data, and performing recursive accumulation by taking signal energy as a value function to obtain a target track. And setting the state transition number of the dynamic programming to be 3, accumulating 500 frames in a recursion manner, and selecting the state of the highest value function as a possible track of the target.
Step two, extracting the track echo, and iteratively optimizing the frequency spectrum image entropy by using a Newton method:
extracting the echo signal of the target, and setting the motion compensation amount a of each step 1 ,a 2 ,a 3 The initial values are all 0, the spectrum is obtained by performing FFT after the compensation by the initial values, and the initial spectrum distribution is shown in FIG. 3. It can be seen that the spectrum of the target is spread and the signal to noise ratio is very low, about 9dB, and difficult to detect. Using Newton's method, for higher order components a 2 ,a 3 The iteration is carried out for 1000 times, as shown in figure 4, finally a 2 ,a 3 Gradually converge to the true value [0.3,0.1 ]]. And finally, detecting after compensating the frequency spectrum by using the motion components obtained by iteration, as shown in fig. 5, greatly enhancing the signal-to-noise ratio of the target frequency spectrum, reaching 27.2dB, and consuming 9 s.
And we utilize a theoretically optimal coherent accumulation algorithm: GRFT, performing third-order motion search compensation, performing accumulation detection under the same hardware condition, wherein the weak target signal-to-noise ratio after accumulation is 28.3dB, but the time is 4300 s. The results of the specific comparisons of the two methods are shown in table 2:
TABLE 2 DP-MIE vs GRFT examples
Evaluation index DP-MIE GRFT
Cumulative signal-to-noise ratio 27.2dB 28.3dB
Operation time consumption 9s 4300s
It can be seen that the method of the present invention loses a very small accumulated gain, but greatly improves the operation efficiency, and verifies the real-time performance and the effectiveness.
The method can be applied to long-time coherent accumulation of radars and realizes efficient detection of maneuvering weak targets.
The present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof, and it will be understood by those skilled in the art that various changes and modifications may be made herein without departing from the spirit and scope of the invention as defined in the appended claims.

Claims (4)

1. A maneuvering weak target detection method based on dynamic programming and minimum image entropy is characterized by comprising the following steps:
s1: receiving K frames of radar echo signals, and acquiring a track of a weak target with the maximum echo energy from the K frames of radar echo signals by adopting a dynamic programming method, wherein each frame of radar echo signal corresponds to one frame of one-dimensional range profile, the one-dimensional range profile comprises a plurality of range units, and the track is formed by the range units of the weak target in each frame of one-dimensional range profile; the method for acquiring the track of the weak target with the maximum echo energy from the K frames of radar echo signals by adopting the dynamic programming method comprises the following steps:
s11: initial value of the set-point function
Figure FDA0003657564770000011
Figure FDA0003657564770000012
Wherein,
Figure FDA0003657564770000013
the state of the nth range cell in the one-dimensional range profile corresponding to the 1 st frame of radar echo signal is shown, and the state comprises a target and no target,
Figure FDA0003657564770000014
the square of the amplitude of the radar echo signal of the nth range unit in the one-dimensional range profile corresponding to the 1 st frame of radar echo signal is obtained;
s12: according to the initial value of the value function corresponding to each distance unit in the 1 st stage, iterative calculation is carried out by adopting the following formula to obtain the value function corresponding to each distance unit from the 2 nd stage to the K th stage
Figure FDA0003657564770000015
Wherein, every stage all acquires a frame radar echo signal:
Figure FDA0003657564770000016
Figure FDA0003657564770000017
wherein,
Figure FDA0003657564770000018
the state of the nth range cell in the one-dimensional range profile corresponding to the kth frame radar echo signal is shown, and the state includes a target and no target, K is 1,2, …, K,
Figure FDA0003657564770000019
is the square of the amplitude of the radar echo signal of the nth range unit,
Figure FDA00036575647700000110
is the most probable transition to the state in all the states of the k-1 stage
Figure FDA00036575647700000111
A state of (1), and
Figure FDA00036575647700000112
all possibilities in the k-1 stageTransition to a State
Figure FDA00036575647700000113
Max is a function taking the maximum value, arg denotes the number of states that will be processed
Figure FDA00036575647700000114
Taking the corresponding state at the time of maximum value as
Figure FDA00036575647700000115
Representation collection
Figure FDA0003657564770000021
The value function corresponding to all the states;
s13: recording the state corresponding to the maximum value of the value function obtained in the K stage as
Figure FDA0003657564770000022
Wherein n is 0 Is in a state
Figure FDA0003657564770000023
The serial number of the located distance unit;
s14: based on the state of the K stage
Figure FDA0003657564770000024
Obtaining the most probable transition to State in stage K-1
Figure FDA0003657564770000025
State of (1)
Figure FDA0003657564770000026
Then, the most possible transition to the state in the K-2 stage is obtained
Figure FDA0003657564770000027
State of (1)
Figure FDA0003657564770000028
In this way, until the stage 1 is traced back, the track of the weak target with the maximum echo energy is obtained;
s2: extracting echo data corresponding to each distance unit where the weak target is located, and then constructing a track echo signal s corresponding to the weak target according to the extracted echo signals DP (k):
Figure FDA0003657564770000029
Wherein A is r For a set target amplitude, λ is the radar wavelength, T is the pulse repetition period of the radar, a 1 ~a H H is 1,2, …, H is a set order, j is an imaginary part, K is 1,2, …, K;
s3: for the track echo signal s DP (k) Performing phase compensation and fourier transform to obtain a compensated spectrum s (m):
Figure FDA00036575647700000210
wherein m is a frequency point,
Figure FDA00036575647700000211
is a phase compensation amount, and
Figure FDA00036575647700000212
s4: obtaining the image entropy E of the spectrum s (m):
Figure FDA00036575647700000213
wherein C is a set constant;
s5: the following objective function is constructed according to the image entropy E:
Figure FDA0003657564770000031
wherein a ═ a 2 ,...,a h ,...,a H ];
S6: let a be 1 When the value is equal to 0, then the objective function is solved by adopting Newton method to obtain undetermined coefficient a 1 ~a H To obtain the final spectrum S end (m);
S7: obtaining a spectrum S end (m) peak value S end (m 0 ) Wherein m is 0 Is a peak value S end (m 0 ) The frequency point of the position;
s8: determine | S end (m 0 )| 2 Whether the threshold value is less than the set CA-CFAR threshold value V T If the weak target is smaller than the target, the weak target is a false alarm target, and if the weak target is not smaller than the target, the weak target is a real target.
2. The method for detecting the maneuvering weak target based on the dynamic programming and the minimum image entropy as claimed in claim 1, characterized in that the setting method of the setting constant C is as follows:
Figure FDA0003657564770000032
3. the method for detecting maneuvering weak targets based on dynamic programming and minimum image entropy as claimed in claim 1, characterized in that the CA-CFAR threshold V is T The setting method comprises the following steps:
Figure FDA0003657564770000033
wherein, P fa In order to set the false alarm rate, R is 1,2, …, R is the number of reference frequency points, S end (m r ) Is a reference frequency point m r The reference frequency point obtaining method comprises the following steps:
at frequency point m 0 Taking a set number of frequency points on the left side and the right side of the center as protection frequency points;
the protection frequency points at the outermost peripheries of the left side and the right side are respectively taken as starting points and extend to the left side and the right side, and the frequency points with the set number on the left side and the right side are taken as reference frequency points.
4. The maneuvering weak target detection method based on dynamic programming and minimum image entropy as claimed in claim 1, characterized in that the objective function is solved by Newton method to obtain undetermined coefficient a 1 ~a H The value of (b) specifically comprises the following steps:
s61: let a be [ a ] 2 ,...,a h ,...,a H ]Is 0, the initial value of the image entropy E is obtained, then the coefficient updating operation is executed on the initial value of the image entropy E, and the updated undetermined coefficient a is obtained 2 ~a H (ii) a Wherein the coefficient updating operation specifically comprises:
s61 a: respectively with a 2 ~a H For variable, obtaining image entropy E to-be-determined coefficient a 2 ~a H First partial derivative of
Figure FDA0003657564770000041
Figure FDA0003657564770000042
Figure FDA0003657564770000043
Wherein, Imag represents an imaginary part, and one represents conjugation;
s61 b: treating a fixed coefficient a based on image entropy E 2 ~a H First partial derivative of
Figure FDA0003657564770000044
Obtaining the entropy E of the image to be determinedCoefficient a 2 ~a H Second partial derivative of
Figure FDA0003657564770000045
Figure FDA0003657564770000046
Wherein,
Figure FDA0003657564770000047
and l represents the amount of phase compensation in the second partial derivative
Figure FDA0003657564770000048
The serial number of (2);
s61 c: calculating the cross term in the second partial derivative according to whether k and l are equal
Figure FDA0003657564770000049
Wherein when k is l:
Figure FDA0003657564770000051
wherein Re represents a real part, and IDFT represents inverse discrete Fourier transform;
when k ≠ l:
Figure FDA0003657564770000052
s61 d: the first partial derivative
Figure FDA0003657564770000053
And second partial derivative
Figure FDA0003657564770000054
Are respectively marked as
Figure FDA0003657564770000055
Figure FDA0003657564770000056
Then according to
Figure FDA0003657564770000057
And
Figure FDA0003657564770000058
updating the undetermined coefficient a 2 ~a H
Figure FDA0003657564770000059
Wherein,
Figure FDA00036575647700000510
is a coefficient to be determined h The iteration value obtained in the (i + 1) th iteration,
Figure FDA00036575647700000511
is a coefficient to be determined h The iteration value obtained in the ith iteration, I is the iteration number, and I is 0,1,2, …, I is the set upper limit value of the iteration number,
Figure FDA00036575647700000512
is a ═ a 2 ,...,a h ,...,a H ]0;
s62: judging the updated undetermined coefficient a 2 ~a H Whether the iteration termination condition is met or not, if any iteration termination condition is met, the undetermined coefficient a obtained by the iteration is obtained 2 ~a H If the values are not satisfied, the step S63 is entered, where the iteration termination condition is:
each coefficient to be determined a 2 ~a H Corresponding first derivative
Figure FDA0003657564770000061
The absolute values of the difference values with 0 are all smaller than a set threshold value;
the iteration times reach an iteration time upper limit value I;
s63: adopting the updated undetermined coefficient a 2 ~a H Updating the image entropy E, and then re-executing the coefficient updating operation on the updated image entropy E to obtain a secondary updated undetermined coefficient a 2 ~a H (ii) a And so on until the updated undetermined coefficient a 2 ~a H An iteration end condition is reached.
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