CN104237853B - A kind of for the particle filter method of trace point mark sequence before multi frame detection - Google Patents
A kind of for the particle filter method of trace point mark sequence before multi frame detection Download PDFInfo
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- CN104237853B CN104237853B CN201410475005.XA CN201410475005A CN104237853B CN 104237853 B CN104237853 B CN 104237853B CN 201410475005 A CN201410475005 A CN 201410475005A CN 104237853 B CN104237853 B CN 104237853B
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- 239000002245 particle Substances 0.000 title claims abstract description 82
- 238000000034 method Methods 0.000 title claims abstract description 61
- 238000001514 detection method Methods 0.000 title claims abstract description 60
- 238000005259 measurement Methods 0.000 claims description 26
- 239000011159 matrix material Substances 0.000 claims description 14
- 238000012952 Resampling Methods 0.000 claims description 12
- 238000012546 transfer Methods 0.000 claims description 6
- 238000004088 simulation Methods 0.000 claims description 5
- 230000017105 transposition Effects 0.000 claims description 2
- 238000012545 processing Methods 0.000 abstract description 6
- 238000007689 inspection Methods 0.000 abstract description 5
- 238000004364 calculation method Methods 0.000 abstract description 2
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- 235000009566 rice Nutrition 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 description 4
- 230000009466 transformation Effects 0.000 description 2
- 238000006424 Flood reaction Methods 0.000 description 1
- 238000000342 Monte Carlo simulation Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005094 computer simulation Methods 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000010606 normalization Methods 0.000 description 1
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
- G01S7/41—Details 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
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Abstract
The present invention provides a kind of for the particle filter method of trace point mark sequence before multi frame detection.Before the domestic invention of this law rice utilizes multi frame detection, tracking processes the short flight path that obtains and is filtered dbjective state processing, and can improve the precision to Target state estimator;Tracking before multi frame detection is processed the short flight path obtained be further processed, it is achieved that the long-time tracking to target, the problem that before solving multi frame detection, tracking is not provided that target complete flight path information;Can dbjective state is estimated in real time with iteration, and do not introduce too much amount of storage and amount of calculation;Predicted by particle state, the missing inspection problem being likely to occur can be followed the tracks of before effectively solving low signal-to-noise ratio dim target detection, it is ensured that the seriality of flight path.
Description
Technical field
The invention belongs to radar data processing technology field, it is particularly to radar weak target tracking technique field.
Background technology
The complexity day by day of radar detection environment is increasingly mature with target stealth technology so that radar timely and reliably monitors and floods
Weak target in strong clutter becomes more difficult.Improve radar and the detecting and tracking performance of weak target is had important theory
It is worth and practical significance.
Before detection, tracking technique is a kind of a kind of technology that weak target carries out in low signal-to-noise ratio environment detecting and tracking.With tradition
Detection method different, follow the tracks of not single frames before detection and announce measurement, but after many frame data are processed, announce mesh simultaneously
Target measurement and flight path.Before realizing detection, the method for tracking technique includes particle filter, dynamic programming, Hough transformation etc..
Before detection based on particle filter, the track initiation ability of tracking is not as the method such as dynamic programming and Hough transformation, and the party
Method needs calculating probability, computationally intensive.But, before the multi frame detection such as dynamic programming, tracking processes and once can only obtain target
Short flight path, it is impossible to obtain the complete flight path of target.And, before some multi frame detections, tracking obtains at discrete space
State estimation result, there is certain loss in estimated accuracy.
Summary of the invention
The technical problem to be solved is, for improving the estimated accuracy to dbjective state, it is provided that one is used for processing multiframe
The filtering method of the short flight path obtained is followed the tracks of before detection.
The present invention solves that above-mentioned technical problem be employed technical scheme comprise that, a kind of for trace point mark sequence before multi frame detection
Particle filter method, comprises the following steps:
Step 1) initialization of variable:
Before initializing total simulation time K, one-time detection, tracking processes frame number N;Before detection, tracking processes thresholding VT, detection before with
Before track measurement possible range γ, a multi frame detection, tracking processes the detection probability of n-th frameRadar scanning
Cycle T, dbjective state transfer matrix F, observing matrix H, process noise covariance Q, population Ns, x and y direction
Distance range [xmin,xmax] and [ymin,ymax], the velocity interval in x and y directionWith
Step 2) particle collectionInitialize:
Initialization time variable k=1 and i-th particle stateIn position, x and y directionAnd speed state Represent transposition;
After initialization particle collection has initialized, enter step 4);
Step 3) status predication:
The particle set pair k moment utilizing the k-1 moment is predicted:Obtain predicting grain
Subset Being the process noise of process noise covariance Q, F is dbjective state transfer matrix;
When in i-th particle state, maximum magnitude value more than its maximum magnitude, is then assigned to this element, and arranges this grain by element
The weights that son is corresponding are set to 0;
Step 4) before multi frame detection tracking process:
Kth-N+1, k-N+2 is read from radar receiver ..., k frame echo data, as k≤N, then from radar receiver
Read the 1,2nd ..., k frame echo data;In tracking process before kth time detection, there is measurement, then enter step 5), no
Then enter step 7);There is measurement and i.e. represent that measurement exceedes thresholding;
Step 5) right value update:
K≤N, then measurement isThe most more new particle weights:
Work as k > N, measurement isStart more new particle weights:
Represent that the last frame moment is tkDetection before tracking process the l frame measurement that obtains,RepresentCorresponding
The state of father's particle, as l≤k-1, usesRepresentThe state of corresponding father's particle;P represents likelihood probability;
Representing and round downwards, H is observing matrix, measuring range variable △xAnd △ySpan beAnd △xAnd △yAll it is not equal to zero;The meter of likelihood probability when γ=1
Without middle entry in formula;
Calculate update after particle weights andAgain to particle weights normalizedEnter
Enter step 6)
Step 6) to the particle collection after right value updateCarry out system resampling;
6.1) initialize
6.2) for all i=2,3 ..., Ns, calculate
6.3) random number u is produced1, u1ObeyIn the range of be uniformly distributed;
6.4) i=1 is made, for all j=1,2 ..., Ns, perform calculating:
Work as uj>ci, then update i=i+1, return step 6.4) until uj≤ci;Make againAnd remember
Record the father particle i of this particlej=i;
Particle set representations after resampling isEnter step 7)
Step 7) Target state estimator:
To the particle state after all resamplingsWeighted averageObtain the Target state estimator result in kth moment;
Step 8) update k=k+1, as k≤K, return step 3), otherwise N frame particle filter terminates.
The present invention passes through above step, it is possible to processes, according to tracking before detection, the short flight path obtained and estimates the most in real time
Dbjective state, obtains the complete flight path of target.
The invention has the beneficial effects as follows, before the present invention utilizes multi frame detection, tracking processes the short flight path that obtains and filters dbjective state
Ripple processes, and can improve the precision to Target state estimator;Tracking before multi frame detection is processed the short flight path obtained do further
Process, it is achieved that the long-time tracking to target, before solving multi frame detection, tracking is not provided that target complete flight path information
Problem;Can dbjective state is estimated in real time with iteration, and do not introduce too much amount of storage and amount of calculation;Pass through
Particle state is predicted, can follow the tracks of the missing inspection problem being likely to occur before effectively solving low signal-to-noise ratio dim target detection, it is ensured that boat
The seriality of mark.
Accompanying drawing explanation
Fig. 1 is the flow chart of the present invention.
Fig. 2 is that in the embodiment of the present invention, the true flight path of target follows the tracks of, with the application present invention, the targetpath obtained.
Fig. 3 is to apply the inventive method to estimate the target location root-mean-square error of dbjective state in the embodiment of the present invention.
Fig. 4 is to apply the inventive method to estimate the target velocity root-mean-square error of dbjective state in the embodiment of the present invention.
Detailed description of the invention
As it is shown in figure 1, flow process of the present invention is as follows:
Step 1) initialization of variable:
Initialize total simulation time K;Before one-time detection, tracking processes frame number N;Target signal to noise ratio SNR;Before detection, tracking processes
Thresholding VT;Follow the tracks of before detection and measure possible range γ, γ ∈ { δ2;δ=1,2,3,4 ... }, δ represents detector unit number, before detection with
Track measures the scope that not can exceed that between measurement and the real goal of tracking before possible range is expressed as detecting;Multiframe inspection
Before surveying, tracking processes the detection probability of n-th frameDetection probability is known when following the tracks of before detecting;Thunder
Reach scan period T;Dbjective state transfer matrix F;Observing matrix H;Process noise covariance Q;Population Ns;X and y side
To distance range [xmin,xmax] and [ymin,ymax];The velocity interval in x and y directionWith
Step 2) particle collectionInitialize:
Initialization time variable k=1 and i-th particle stateIn position, x and y directionAnd speed state
Rand (1) represents random according to be uniformly distributed on one [0,1] interval of generation
Number;
I-th particle weightsIt is initialized as:
After particle collection has initialized, enter step 4);
Step 3) status predication:
The particle set pair k moment utilizing the k-1 moment is predicted:Obtain predicting grain
Subset It it is the process noise of process noise covariance Q;
When in i-th particle state, maximum magnitude value more than its maximum magnitude, is then assigned to this element, and arranges this grain by element
The weights that son is corresponding are set to 0;
Step 4) before multi frame detection tracking process:
Kth-N+1, k-N+2 is read from radar receiver ..., k frame echo data, as k≤N, then from radar receiver
Read the 1,2nd ..., k frame echo data;In tracking process before kth time detection, there is measurement, then enter step 5), no
Then enter step 7);
Step 5) right value update:
K≤N, then measurement isThe most more new particle weights:
Work as k > N, measurement isStart more new particle weights:
Represent that the last frame moment is tkDetection before tracking process the l frame measurement that obtains,RepresentCorresponding
The state of father's particle, as l≤k-1, usesRepresentThe state of corresponding father's particle;P represents
Likelihood probability;
Representing and round downwards, H is observing matrix, measuring range variable △xAnd △ySpan beAnd △xAnd △yAll it is not equal to zero;
Calculate update after particle weights andAgain to particle weights normalizedEnter
Enter step 6)
Step 6) to the particle collection after right value updateCarry out system resampling;
6.1) initialize
6.2) for all i=2,3 ..., Ns, calculate
6.3) random number u is produced1, u1ObeyIn the range of be uniformly distributed;
6.4) i=1 is made, for all j=1,2 ..., Ns, perform calculating:
Work as uj>ci, then update i=i+1, return step 6.4) until uj≤ci;Make againAnd remember
Record the father particle i of this particlej=i;
Particle set representations after resampling isEnter step 7)
Step 7) Target state estimator:
To the particle state after all resamplingsWeighted averageObtain the Target state estimator result in kth moment;
Step 8, renewal k=k+1, as k≤K, return step 3), otherwise N frame particle filter terminates.
Embodiment
The present invention mainly uses the method for Computer Simulation to verify, institute is in steps, conclusion is all on MATLAB-R2010b
Checking is correct.It is embodied as step as follows:
Step 1, initialization of variable:
Initializing variable includes: total simulation time K=30;Before one-time detection, tracking processes frame number N=6;Target signal to noise ratio
SNR=8dB;Before detection, tracking processes thresholding VT=13.2847;Follow the tracks of before detection and measure possible range γ=72;Multiframe inspection
Before surveying, tracking processes the 1,2nd ..., the detection probability of N frame is respectively 0.876,0.892,0.918,0.910,0.908,0.838;Radar scanning
Cycle T=1s;Dbjective state transfer matrix F
Observing matrix H
Process noise covariance Q
Population Ns=8000;The distance range in x and y direction is [1,59];The velocity interval in x and y direction is [0.6,1.2].
Step 2, particle collection initialize:
Initialization time variable k=1.Particle x and position, y direction and speed state initialize
Wherein rand (1) represents according to being uniformly distributed the random number produced on [0,1] interval.Order
Particle weight initialization
Then, primary collection is obtained
Step 3, status predication:
If k=1, then skip this step.Otherwise the particle collection in k-1 moment is carried out one-step prediction
Obtain predicting particle collectionWhereinBe average be null covariance matrix be the process noise of Q.
If i-th particle stateOrThen makeOrIfOrThen makeOrAnd weights corresponding for this particle are set to
0。
Before step 4, multi frame detection, tracking processes:
Kth-N+1, k-N+2 is read from radar receiver ..., and k frame echo data (if k≤N, then from radar receiver
Middle reading the 1st, 2 ..., N frame echo data), before carrying out multi frame detection, tracking processes.
Step 5, right value update:
OrderRepresent that the last frame moment is tkDetection before tracking process the l frame measurement that obtains.If this detection
Measurement is there is in front tracking in processingIf (k≤N, then measurement is), then update and predict particle weights:
Convenient in order to represent, useRepresentThe state of corresponding father's particle, as l≤k-1, usesRepresentCorresponding father's grain
The state of son.As k > N time, the most more new particle weights
Wherein, likelihood probability
△xAnd △ySpan beAnd △xAnd △yAll it is not equal to zero.
As k≤N, the most more new particle weights
Calculate particle weights and
To particle weights normalization in the case of Ξ is not zero
If tracking does not exist measurement in processing before this detection, i.e. do not have state to cross thresholding, then skip this step.
Step 6, resampling:
If tracking does not exist measurement in processing before this detection, i.e. do not have state to cross thresholding, then skip this step.No
Then to the particle collection after right value updateCarry out system resampling.
6.1, initialize
6.2, for all i=2,3 ..., Ns, calculate
6.3, u is randomly generated1, it is obeyedIn the range of be uniformly distributed, i.e.
6.4, i=1 is made, for all j=1,2 ..., Ns, perform calculated below:
If uj>ci, then circulation performs i:=i+1, until uj≤ci.Then makeAnd record this particle
Father particle ij=i.
Particle set representations after resampling is
Step 7, Target state estimator:
To all particle statesWeighted averageObtain the Target state estimator result in kth moment.
Step 8, make k:=k+1, if k≤K, repeat step 3~step 7.
Accompanying drawing 2 gives the restoration result in this simulation example to targetpath, successfully provides the complete flight path of target
Information, and there is not missing inspection problem.Accompanying drawing 3 gives the target location root-mean-square error utilizing the present invention to obtain in the present embodiment,
Accompanying drawing 4 gives the target velocity root-mean-square error utilizing the present invention to obtain in the present embodiment, is 200 Monte Carlo experiments
Statistical result, result shows that the method has higher and stable estimated accuracy.
Claims (2)
1. one kind for the particle filter method of trace point mark sequence before multi frame detection, it is characterised in that comprise the following steps:
Step 1) initialization of variable:
Before initializing total simulation time K, one-time detection, tracking processes frame number N;Before detection, tracking processes thresholding VT, detection before with
Before track measurement possible range γ, a multi frame detection, tracking processes the detection probability of n-th frameN=1,2 ..., N, radar scanning
Cycle T, dbjective state transfer matrix F, observing matrix H, process noise covariance Q, population Ns, x and y direction
Distance range [xmin,xmax] and [ymin,ymax], the velocity interval in x and y directionWith
Step 2) particle collectionInitialize:
Initialization time variable k=1 and i-th particle stateIn position, x and y directionAnd speed state [·]TRepresent transposition;
After initialization particle collection has initialized, enter step 4);
Step 3) status predication:
The particle set pair k moment utilizing the k-1 moment is predicted:Obtain predicting grain
Subset Being the process noise of process noise covariance Q, F is dbjective state transfer matrix;
When in i-th particle state, maximum magnitude value more than its maximum magnitude, is then assigned to this element, and arranges this grain by element
The weights that son is corresponding are set to 0;
Step 4) before multi frame detection tracking process:
Work as k > N, from radar receiver, read kth-N+1, k-N+2 ..., k frame echo data, as k≤N, then from thunder
Reach and receiver read the 1,2nd ..., N frame echo data;In tracking processes before kth time detection, there is measurement, then enter
Step 5), otherwise enter step 7);There is measurement and i.e. represent that measurement exceedes tracking process thresholding V before detectionT;
Step 5) right value update:
K≤N, then measurement isThe most more new particle weights:
Work as k > N, measurement isStart more new particle weights:
Represent that the last frame moment is tkDetection before tracking process the l frame measurement that obtains,RepresentCorresponding
The state of father's particle, as l≤k-1, usesRepresentThe state of corresponding father's particle;P represents likelihood probability;
Representing and round downwards, H is observing matrix, measuring range variable ΔxAnd ΔySpan beAnd ΔxAnd ΔyAll it is not equal to zero;The meter of likelihood probability when γ=1
Without middle entry in formula;
Calculate update after particle weights andAgain to particle weights normalizedEnter
Enter step 6)
Step 6) to the particle collection after right value updateCarry out system resampling;
6.1) initialize
6.2) for all i=2,3 ..., Ns, calculate
6.3) random number u is produced1, u1ObeyIn the range of be uniformly distributed;
6.4) i=1 is made, for all j=1,2 ..., Ns, perform calculating:
Work as uj>ci, then update i=i+1, return step 6.4) until uj≤ci;Make againAnd remember
Record the father particle i of this particlej=i;
Particle set representations after resampling isEnter step 7)
Step 7) Target state estimator:
To the particle state after all resamplingsWeighted averageObtain the Target state estimator result in kth moment;
Step 8) update k=k+1, as k≤K, return step 3), otherwise N frame particle filter terminates.
It is a kind of for the particle filter method of trace point mark sequence before multi frame detection, it is characterised in that
Initialization time variable k=1 and i-th particle stateIn position, x and y directionAnd speed state
Method particularly includes:
Rand (1) represents according to being uniformly distributed the random number produced on [0,1] interval;
Initialize i-th particle weightsConcrete grammar for for:
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CN107656265A (en) * | 2017-09-19 | 2018-02-02 | 电子科技大学 | Particle filter fusion method for tracking short flight path before multi frame detection |
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CN105137419B (en) * | 2015-09-09 | 2017-08-11 | 电子科技大学 | Tracking before a kind of particle filter detection of utilization graing lobe gain |
CN106226750B (en) * | 2016-07-01 | 2018-06-19 | 电子科技大学 | A kind of point mark sequence smooth filtering method for multi-frame joint detection |
CN107037424B (en) * | 2017-04-24 | 2020-02-18 | 电子科技大学 | Doppler radar multi-frame pre-coherent detection tracking method based on sequential optimization |
CN107340517B (en) * | 2017-07-04 | 2021-02-05 | 电子科技大学 | Multi-sensor multi-frame tracking-before-detection method |
CN108333571B (en) * | 2018-02-07 | 2020-04-21 | 电子科技大学 | Multi-sensor multi-frame joint detection tracking method based on trace point sequence fusion |
CN110673132B (en) * | 2019-10-11 | 2022-01-11 | 电子科技大学 | Real-time filtering method for trace point sequence for multi-frame joint detection and tracking |
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KR101231378B1 (en) * | 2011-08-12 | 2013-02-15 | 숭실대학교산학협력단 | Apparatus and recording media for tracking user location |
CN102621543B (en) * | 2012-04-02 | 2015-02-25 | 中国人民解放军海军航空工程学院 | Dim target track-before-detect method based on particle filter algorithm and track management |
CN102722706B (en) * | 2012-05-24 | 2014-01-29 | 哈尔滨工程大学 | Particle filter-based infrared small dim target detecting and tracking method and device |
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CN107656265B (en) * | 2017-09-19 | 2021-03-30 | 电子科技大学 | Particle filter fusion method for tracking short flight path before multi-frame detection |
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