CN106707269A - Radar object speed tracking method based on cross-product automatic frequency control - Google Patents
Radar object speed tracking method based on cross-product automatic frequency control Download PDFInfo
- Publication number
- CN106707269A CN106707269A CN201510781236.8A CN201510781236A CN106707269A CN 106707269 A CN106707269 A CN 106707269A CN 201510781236 A CN201510781236 A CN 201510781236A CN 106707269 A CN106707269 A CN 106707269A
- Authority
- CN
- China
- Prior art keywords
- data point
- cross product
- frequency
- signal
- formula
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- 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
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S13/50—Systems of measurement based on relative movement of target
- G01S13/58—Velocity or trajectory determination systems; Sense-of-movement determination systems
-
- 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
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/66—Radar-tracking systems; Analogous systems
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
The invention provides a radar object speed tracking method based on cross-product automatic frequency control. A cross-product automatic frequency control method is used to measure target Doppler frequency difference, a measured value is sent to a loop filter, the object speed in a next coherent processing interval is predicted, and a speed tracking loop is formed. According to the method, the problem that the tracking precision relies on the resolution of rapid Fourier transform is overcome, the problem of deficiency in a data filtering function is solved, and the method is low in errors and high in precision.
Description
Technical field
The invention belongs to radar target tracking technical field, and in particular to a kind of radar mesh based on the control of cross product automatic frequency
Mark speed tracing method.
Background technology
Traditional radar target speed tracing method is the narrow band signal by radar speed passage by Fast Fourier Transform (FFT)
After (Fast Fourier Transformation, FFT), the tracking to target Doppler is realized using height tracking filter,
And then the pursuit gain of target velocity is obtained, it is achieved in tracking of the radar to target velocity.
This method is primarily present two shortcomings, radar can be caused low to the tracking accuracy of target velocity and tracking error
Greatly.(1) tracking accuracy of conventional speed tracking depends on FFT resolution ratio, and can on hardware signal processing platform
The FFT resolution ratio of offer is limited so that limited precision of the conventional speed tracking to tachometric survey;(2) tradition
Current velocity measurement is only used in speed tracing method, data filtering has not been carried out to several measured values before
Treatment, the adjacent value of speed tracing twice generally differs larger, and the burr of speed tracing curve is more, causes tracking error big.
The content of the invention
It is an object of the invention to provide a kind of radar target speed tracing method based on the control of cross product automatic frequency, the party
Method error is small, high precision.
In order to solve the above-mentioned technical problem, the present invention provide it is a kind of based on cross product automatic frequency control radar target speed with
Track method, comprises the following steps:
The first step, the data point of radar speed channel signal is extracted using sliding window, obtains M data point;
Second step, Frequency mixing processing is carried out by M data point by digital controlled oscillator, the signal after being mixed;
3rd step, real part treatment is taken to the signal after mixing and imaginary part treatment is taken respectively, is obtained solid part signal and is believed with imaginary part
Number;
4th step, according to the solid part signal and imaginary signals, mixed signal is calculated according to cross product computational methods respectively
The M cross product value of data point, and the cross product value of M data point is added up, obtain cross product energy and P;Simultaneously with modulus
Mode calculates mixed signal the corresponding modulus value of M data point of acquisition respectively, and obtains M data point mould to calculating
The average A of value;
5th step, the slope K for obtaining frequency discrimination curve is calculated using cross product auto frequency control method, and according to described oblique
Rate K is calculated and is obtained Doppler's frequency difference on the frequency dfd;
6th step, by Doppler frequency difference dfdDoppler frequency difference df is obtained in feeding loop filterdFilter value;So
Afterwards by Doppler frequency difference dfdFilter value feeding digital controlled oscillator in obtain Doppler frequency filter value fd;
7th step, judges whether all to extract all signal datas for finishing radar speed passage using sliding window, if extracted
Complete whole signal datas, then the filter value f of the Doppler frequency that will be obtaineddOutput, and enter the 8th step;Otherwise return to
One step.
8th step, calculates and obtains the pie slice value v of radar target, shown in computational methods such as formula (1):
In formula (1), λ is radar operation wavelength.
Further, shown in the computational methods such as formula (2) of cross product value described in the 4th step,
Pt(k)=Ik-1·Qk-Qk-1·Ik (2)
In formula (2), PtK () is the corresponding cross product value of k-th data point, IkIt is k-th solid part signal of data point,
QkIt is k-th imaginary signals of data point, k ∈ M.
Further, shown in the computational methods such as formula (3) of modulus value described in the 4th step,
In formula (3), AtK () is the corresponding modulus value of k-th data point, I in mixed signalkIt is k-th data point
Solid part signal, QkIt is k-th imaginary signals of data point, k ∈ M.
Further, shown in the calculation such as formula (4) of the slope K of frequency discrimination curve described in the 5th step:
In formula (4), T is the time interval of the data point that radar speed channel signal is extracted using sliding window.
Further, Doppler's frequency difference on the frequency df described in the 5th stepdComputational methods such as formula (5) shown in:
Compared with prior art, its remarkable advantage is that the present invention is using cross product auto frequency control method (Cross to the present invention
Product Automatic Frequency Control, CPAFC) measurement of the realization to target Doppler frequency difference, then will be many
In the general measured value feeding loop filter for strangling frequency difference, next coherent processing interval (Coherent Processing are predicted
Interval, CPI) target velocity, be consequently formed speed tracing loop, so as to solve conventional radar target velocity tracking
The tracking accuracy of method need to rely on FFT resolution ratio, and data filtering afunction problem.
Brief description of the drawings
Fig. 1 is radar target speed tracing method flow schematic diagram of the present invention based on the control of cross product automatic frequency.
Fig. 2 is to use in the present invention sliding window to extract the schematic diagram of radar speed channel signal data point.
Fig. 3 is the schematic diagram of a scenario of the Computer Simulation in emulation experiment of the present invention.
Fig. 4 is the speed change curves schematic diagram of radar target in emulation experiment of the present invention.
Fig. 5 is that the inventive method is shown with the tracking performance correlation curve of speed tracing method of the tradition based on fast Fourier transformation
It is intended to.
Specific embodiment
It is readily appreciated that, according to technical scheme, in the case where connotation of the invention is not changed, this area
Those skilled in the art can imagine radar target speed tracing method of the present invention based on the control of cross product automatic frequency
Numerous embodiments.Therefore, detailed description below and accompanying drawing are only the exemplary illustrations to technical scheme,
And be not to be construed as whole of the invention or be considered as limitation or restriction to technical solution of the present invention.
With reference to Fig. 1, radar target speed tracing method of the present invention based on the control of cross product automatic frequency is comprised the following steps:
The first step, the data point of radar speed channel signal is extracted using sliding window, obtains M data point.Such as Fig. 2 institutes
Show, since radar speed passage first data point of signal, M data point is extracted using sliding window, obtain this
The data point for the treatment of needed for secondary coherent processing interval (CPI).Next CPI extract data point when, sliding window order to
A data point is moved afterwards, obtains M corresponding data point of next CPI.
Second step, Frequency mixing processing is carried out by M data point by digital controlled oscillator, the signal after being mixed.
3rd step, real part treatment is taken to the signal after mixing and imaginary part treatment is taken respectively, obtains solid part signal I and imaginary part
Signal Q.
4th step, the cross product value of M data point of mixed signal, calculating side are calculated according to cross product computational methods respectively
Shown in method such as formula (1),
Pt(k)=Ik-1·Qk-Qk-1·Ik (1)
In formula (1), PtK () is the corresponding cross product value of k-th data point, IkK-th data point that step 3 is obtained
Solid part signal, QkIt is the imaginary signals of k-th data point that step 3 is obtained, k ∈ M.
5th step, by the M cross product value P of data pointtK () is added up, obtain corresponding cross product energy and P, cross product energy
With P such as formulas (2) Suo Shi:
6th step, the corresponding modulus value of M data point is calculated mixed signal in modulus mode respectively, and computational methods are such as
Shown in formula (3),
In formula (3), AtK () is the corresponding modulus value of k-th data point in mixed signal.
7th step, calculates M data point modulus value AtThe average A of (k), shown in computational methods such as formula (4):
8th step, the slope K for obtaining CPAFC frequency discrimination curves, calculating side are calculated using cross product auto frequency control method
Shown in formula such as formula (5):
In formula (5), T is the time interval of the data point that radar speed channel signal is extracted using sliding window.
9th step, calculates and obtains Doppler's frequency difference on the frequency dfd, shown in computational methods such as formula (6):
Tenth step, by Doppler frequency difference dfdIn feeding loop filter, Doppler frequency difference df is obtaineddFilter value.
11st step, will obtain the filter value of Doppler frequency in the filter value feeding digital controlled oscillator of Doppler frequency difference
fd。
12nd step, judges whether all to extract all signal datas for finishing radar speed passage using sliding window, if carried
Total data is taken, then the filter value f of the Doppler frequency that will be obtaineddOutput, and enter the 13rd step;Otherwise return to
One step.
13rd step, calculates and obtains the pie slice value v of radar target, shown in computational methods such as formula (7):
Formula (7), λ is radar operation wavelength.
The present invention can be further illustrated by following emulation experiment.
With reference to Fig. 3, target maneuver flight, radar and target move toward one another, wherein, target moves along a curved path, and radar is made
Linear motion.Fig. 4 be Computer Simulation scene between radar and target radial velocity change curve.Fig. 5 gives
In the Computer Simulation scene shown in Fig. 3, using the inventive method and speed tracing side of the tradition based on Fourier transformation
The speed tracing performance comparison curve of method.From figure 5 it can be seen that the tracking error of the inventive method is smaller, Er Qiesui
The carrying out of tracking mode, due to not using data filtering in conventional speed tracking, it cannot be accurately pre-
Survey the radial velocity of radar and target in next CPI.Therefore, in the scene of radial velocity acute variation, using height
The speed tracing error of the conventional speed tracking of low Doppler Tracking wave filter is with the change aggravation of radial velocity
Become bigger and bigger, or even occur in that obvious divergent trend.Contrast apparently, the speed tracing error that the inventive method is obtained according to
It is old to maintain a highly desirable level.Using the speed tracing loop of conventional speed tracking, its speed tracing is square
Root error is 1.0981m/s;The speed tracing root-mean-square error that proposition method of the present invention obtains speed tracing loop is 0.0924
M/s, is the 8.4% of control methods, and performance is significantly improved.
Claims (5)
1. it is a kind of based on cross product automatic frequency control radar target speed tracing method, it is characterised in that including following
Step:
The first step, the data point of radar speed channel signal is extracted using sliding window, obtains M data point;
Second step, Frequency mixing processing is carried out by M data point by digital controlled oscillator, the signal after being mixed;
3rd step, real part treatment is taken to the signal after mixing and imaginary part treatment is taken respectively, is obtained solid part signal and is believed with imaginary part
Number;
4th step, according to the solid part signal and imaginary signals, mixed signal is calculated according to cross product computational methods respectively
The M cross product value of data point, and the cross product value of M data point is added up, obtain cross product energy and P;Simultaneously with modulus
Mode calculates mixed signal the corresponding modulus value of M data point of acquisition respectively, and obtains M data point mould to calculating
The average A of value;
5th step, the slope K for obtaining frequency discrimination curve is calculated using cross product auto frequency control method, and according to described oblique
Rate K is calculated and is obtained Doppler's frequency difference on the frequency dfd;
6th step, by Doppler frequency difference dfdDoppler frequency difference df is obtained in feeding loop filterdFilter value;So
Afterwards by Doppler frequency difference dfdFilter value feeding digital controlled oscillator in obtain Doppler frequency filter value fd;
7th step, judges whether all to extract all signal datas for finishing radar speed passage using sliding window, if extracted
Complete whole signal datas, then the filter value f of the Doppler frequency that will be obtaineddOutput, and enter the 8th step;Otherwise return to
One step.
8th step, calculates and obtains the pie slice value v of radar target, shown in computational methods such as formula (1):
In formula (1), λ is radar operation wavelength.
2. the radar target speed tracing method for being controlled based on cross product automatic frequency as claimed in claim 1, its feature is existed
In, shown in the computational methods such as formula (2) of cross product value described in the 4th step,
Pt(k)=Ik-1·Qk-Qk-1·Ik (2)
In formula (2), PtK () is the corresponding cross product value of k-th data point, IkIt is k-th solid part signal of data point,
QkIt is k-th imaginary signals of data point, k ∈ M.
3. the radar target speed tracing method for being controlled based on cross product automatic frequency as claimed in claim 1, its feature is existed
In, shown in the computational methods such as formula (3) of modulus value described in the 4th step,
In formula (3), AtK () is the corresponding modulus value of k-th data point, I in mixed signalkIt is k-th data point
Solid part signal, QkIt is k-th imaginary signals of data point, k ∈ M.
4. the radar target speed tracing method for being controlled based on cross product automatic frequency as claimed in claim 1, its feature is existed
In shown in the calculation such as formula (4) of the slope K of frequency discrimination curve described in the 5th step:
In formula (4), T is the time interval of the data point that radar speed channel signal is extracted using sliding window.
5. the radar target speed tracing method for being controlled based on cross product automatic frequency as claimed in claim 1, its feature is existed
In Doppler's frequency difference on the frequency df described in the 5th stepdComputational methods such as formula (5) shown in:
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510781236.8A CN106707269A (en) | 2015-11-13 | 2015-11-13 | Radar object speed tracking method based on cross-product automatic frequency control |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510781236.8A CN106707269A (en) | 2015-11-13 | 2015-11-13 | Radar object speed tracking method based on cross-product automatic frequency control |
Publications (1)
Publication Number | Publication Date |
---|---|
CN106707269A true CN106707269A (en) | 2017-05-24 |
Family
ID=58930888
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201510781236.8A Pending CN106707269A (en) | 2015-11-13 | 2015-11-13 | Radar object speed tracking method based on cross-product automatic frequency control |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106707269A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109633623A (en) * | 2018-11-30 | 2019-04-16 | 上海无线电设备研究所 | A kind of radar speed track loop design method |
CN109633626A (en) * | 2017-10-05 | 2019-04-16 | 通用汽车环球科技运作有限责任公司 | The method for tracking object |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7053815B1 (en) * | 1981-11-30 | 2006-05-30 | Alenia Marconi Systems Limited | Radar tracking system |
CN104199063A (en) * | 2014-08-20 | 2014-12-10 | 北京遥测技术研究所 | Blind frequency detector processing method based on cross product algorithm |
CN104242928A (en) * | 2014-08-20 | 2014-12-24 | 北京遥测技术研究所 | Frequency locking detector processing method based on cross product algorithm in frequency locking loop |
CN104320201A (en) * | 2014-09-23 | 2015-01-28 | 西安空间无线电技术研究所 | Spatial coherent optical communication high-dynamic carrier capture tracking loop |
-
2015
- 2015-11-13 CN CN201510781236.8A patent/CN106707269A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7053815B1 (en) * | 1981-11-30 | 2006-05-30 | Alenia Marconi Systems Limited | Radar tracking system |
CN104199063A (en) * | 2014-08-20 | 2014-12-10 | 北京遥测技术研究所 | Blind frequency detector processing method based on cross product algorithm |
CN104242928A (en) * | 2014-08-20 | 2014-12-24 | 北京遥测技术研究所 | Frequency locking detector processing method based on cross product algorithm in frequency locking loop |
CN104320201A (en) * | 2014-09-23 | 2015-01-28 | 西安空间无线电技术研究所 | Spatial coherent optical communication high-dynamic carrier capture tracking loop |
Non-Patent Citations (1)
Title |
---|
BINGBING JIANG ET AL.: "CPAFC-Based Radar Seeker Velocity Tracking Loop Design", 《THE FOURTH INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION AND INFORMATION SCIENCES》 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109633626A (en) * | 2017-10-05 | 2019-04-16 | 通用汽车环球科技运作有限责任公司 | The method for tracking object |
CN109633623A (en) * | 2018-11-30 | 2019-04-16 | 上海无线电设备研究所 | A kind of radar speed track loop design method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN104237879B (en) | A kind of multi-object tracking method in radar system | |
CN105068058B (en) | A kind of grade Microstroke measuring method based on synthetic wideband pulse Doppler radar | |
CN110412558A (en) | The vehicle-mounted fmcw radar velocity ambiguity method of solution based on TDM MIMO | |
CN104076353B (en) | A kind of Area Objects echo beam center speed measurement method | |
CN107907878A (en) | The method that high accuracy obtains fmcw radar distance measure | |
CN103616679A (en) | PD radar ranging and angle measuring method based on difference beam modulation and waveform analysis | |
CN106707271A (en) | Adaptive angle tracking method based on digital phase-locked loop | |
CN105137373B (en) | A kind of denoising method of exponential signal | |
CN106707269A (en) | Radar object speed tracking method based on cross-product automatic frequency control | |
CN106054159A (en) | Instantaneous frequency extraction method of Doppler signals | |
CN107064629A (en) | It is a kind of that simple signal frequency estimating methods are integrated based on the segmentation that frequency relative bias is estimated | |
CN108287335A (en) | A method of ranging and range rate being carried out to multiple target using the frequency modulated signal of LFMCW radars | |
CN106546949A (en) | A kind of double array element sinusoidal signal arrival bearing's methods of estimation based on frequency estimation meter | |
CN111007473B (en) | High-speed weak target detection method based on distance frequency domain autocorrelation function | |
CN104793193A (en) | Micro-Doppler time-space-frequency three-dimensional analysis method based on SAR-DPCA (Synthetic Aperture Radar-Data Processing Control Area) | |
CN104200458A (en) | MeanShift based high-resolution remote sensing image segmentation distance measurement optimization method | |
CN107346022B (en) | High-precision ship measuring radar and speed measuring method based on microwave interferometer | |
CN106320255B (en) | A kind of computational methods of Flood Plain Flow swale inflow-rate of water turbine | |
CN106330342A (en) | Water sound communication doppler factor estimation method with low computation complexity | |
CN105117609A (en) | Dynamic weighing method based on generalized K-Means classification decision | |
CN104880697A (en) | Chirp signal parameter estimating method based on sparse constraint | |
CN104977570A (en) | Null-space-tuning-based dual-channel sparse SAR moving target detection improvement method | |
CN108107393A (en) | A kind of spectral peak Credibility judgement method in frequency analysis | |
CN105548987B (en) | A kind of continuous wave radar aimed acceleration blind estimating method | |
DE19914486C1 (en) | Arrangement for contactless speed measurement of an object moving across a surface detects component of combined Doppler spectrum with highest or lowest frequency and power level exceeding defined value |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170524 |
|
RJ01 | Rejection of invention patent application after publication |