CN101598789A - The time unifying method that is used for single or double base complex high-frequency radar nets - Google Patents

The time unifying method that is used for single or double base complex high-frequency radar nets Download PDF

Info

Publication number
CN101598789A
CN101598789A CNA2009100723438A CN200910072343A CN101598789A CN 101598789 A CN101598789 A CN 101598789A CN A2009100723438 A CNA2009100723438 A CN A2009100723438A CN 200910072343 A CN200910072343 A CN 200910072343A CN 101598789 A CN101598789 A CN 101598789A
Authority
CN
China
Prior art keywords
sensor
beta
centerdot
time
curve
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.)
Granted
Application number
CNA2009100723438A
Other languages
Chinese (zh)
Other versions
CN101598789B (en
Inventor
许诺
魏红江
张玉瑶
孔芳园
位寅生
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Harbin Institute of Technology
Original Assignee
Harbin Institute of Technology
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Harbin Institute of Technology filed Critical Harbin Institute of Technology
Priority to CN2009100723438A priority Critical patent/CN101598789B/en
Publication of CN101598789A publication Critical patent/CN101598789A/en
Application granted granted Critical
Publication of CN101598789B publication Critical patent/CN101598789B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The time unifying method that is used for single or double base complex high-frequency radar nets, it relate to high-spectrum remote sensing data emulation with the data fusion technical field, it has solved the detection accuracy and the power of the air missile weapon system of existing employing single target sensor autonomous operation and has reduced greatly, the killing area sharply reduces, cause the air defence weapon system fighting efficiency significantly to descend, even lose the problem of fight capability substantially.If each sensor when starting working, passed through system to the time; In period of time hereafter, each sensor obtains one group of data based on sampling instant.Select the measurement data of sensor, obtain a curve, draw the value of other any times by the curve calculation after the match through data are carried out curve fitting.Utilize this method in the single or double base complex high-frequency radar nets system, also to require to utilize existing equipment to improve the target detection precision as much as possible, to improve the electronic warfare capability of total system.

Description

The time unifying method that is used for single or double base complex high-frequency radar nets
Technical field
The present invention relates to high-spectrum remote sensing data emulation with the data fusion technical field.
Background technology
Since the nineties, the Gulf War, NATO air attack the Federal Republic of Yugoslavia, Afghan War and the war in Iraq have successively taken place in the world from eighties of last century.Make a general survey of these several wars, the offense uses measures such as stealthy scouting, electronic interferences, stealthy bombing and the attack of little radar area cruise missile in a large number, suppress the side's of defence antiaircraft weapon effectively and found, followed the tracks of and measure the ability of target, the feasible detection accuracy and the power of the air missile weapon system of single target sensor autonomous operation of adopting reduced greatly, the killing area sharply reduces, cause the air defence weapon system fighting efficiency significantly to descend, even lose fight capability substantially.In the face of increasingly serious air strike environment, improve the anti-stealthy and antijamming capability of air defence weapon system, keep the overall combat effectiveness of air defence weapon system, be current problem very important and to be solved.
People more and more are concerned about using sensor network monitoring in the past few years.Thereby sensor network can obtain bulk data from the sensor of many independent operatings merges the complementation of formation state, and the sensor network that utilizes multisensor to constitute has advantages such as the reliability of the coverage rate that increases data, enhanced system and robustness.In carrying out data handling procedure, the data-switching that needs localized sensor is recorded for the authentic communication that obtains target is in common coordinate reference system, but owing to have the deviation and the measuring error of sensor, directly change being difficult to guarantee precision and having given play to the superiority of utilizing multisensor, therefore when multi-sensor data is handled, need the registration Algorithm of some sensors.
In the single or double base complex high-frequency radar nets system, also require to utilize existing equipment to improve the target detection precision as much as possible, to improve the electronic warfare capability of total system.
Summary of the invention
The present invention reduces greatly in order to solve the existing detection accuracy and the power of the air missile weapon system of single target sensor autonomous operation of adopting, the killing area sharply reduces, cause the air defence weapon system fighting efficiency significantly to descend, even lose the problem of fight capability substantially, and a kind of time unifying method that is used for single or double base complex high-frequency radar nets has been proposed.
The time unifying method step that is used for single or double base complex high-frequency radar nets of the present invention is as follows:
Step 1: set simulation parameter; Set up rectangular coordinate system with the first base station T as true origin, and the distance of establishing the first base station T and the second base station R is L, set moving target P again, and to establish moving target P initial position be P (L, L), moving target P moves horizontally with the straight line that the speed of vm/s is parallel to the first base station T and R place, second base station; First sensor A among the first base station T is that collection period comes image data with x second, and the second sensor B of the second base station R is that collection period comes image data with y second;
Step 2: carry out emulation according to the simulation parameter in the step 1, and establish first sensor A and the second sensor B when beginning emulation image data, passed through system to the time; In time, the first sensor A and the second sensor B collect one group of sampled data based on the described observed samples time in after this one section observed samples;
Step 3: the measurement data of one or two sensor that is obtained in the selection step 2, through being carried out curve fitting, data obtain a curve, draw the value of other any times by the curve calculation after the match.
Be provided with the first sensor A and the second sensor B, with different frequencies target carried out sampled measurements respectively, each sensor can uniform sampling, also can nonuniform sampling.Each sensor is at sampling instant t 1A measured value is arranged, be designated as (t i, y i), each sensor can obtain one group of measured value like this.Because the sampling period difference of sensor, the time ti value that each sensor obtains data is not quite similar.If directly merge, may make fusion results lose meaning owing to the mistiming, be not so good as the fusion accuracy height of single-sensor on the contrary.Therefore before carrying out data fusion, difference measurement data constantly must be registered on the same time point.
The present invention adopts the time alignment that carries out multisensor based on the method for curve fitting.If each sensor when starting working, passed through system to the time, promptly each sensor carries out measuring the first time to target at one time.This method is used for the emulation of single or double base complex high-frequency radar nets time unifying method data, it has considered that comprehensively thereby sensor network can obtain bulk data and merge the complementation of formation state from the sensor of many independent operatings, and the sensor network that utilizes multisensor to constitute has advantages such as the reliability of the coverage rate that increases data, enhanced system and robustness.Utilize this method in the single or double base complex high-frequency radar nets system, also to require to utilize existing equipment to improve the target detection precision as much as possible, to improve the electronic warfare capability of total system.
Description of drawings
Fig. 1 is the single or double base complex high-frequency radar nets synoptic diagram; Fig. 2 is the observation track plot before the registration; Fig. 3 is the observation track plot behind the registration.
Embodiment
Embodiment one: in conjunction with Fig. 1 present embodiment is described, the present embodiment step is as follows:
Step 1: set simulation parameter; Set up rectangular coordinate system with the first base station T as true origin, and the distance of establishing the first base station T and the second base station R is L, promptly the coordinate at two stations is: T (0,0), R (L, 0); Set moving target P again, and establish moving target P initial position be P (L, L), moving target P moves horizontally with the straight line that the speed of vm/s is parallel to the first base station T and R place, second base station; First sensor A among the first base station T is that collection period comes image data with x second, and the second sensor B of the second base station R is that collection period comes image data with y second;
Step 2: carry out emulation according to the simulation parameter in the step 1, and establish first sensor A and the second sensor B when beginning emulation image data, passed through system to the time, promptly each sensor carries out measurement first time to target at one time; In time, the first sensor A and the second sensor B collect one group of sampled data based on the described observed samples time in after this one section observed samples;
Step 3: the measurement data of one or two sensor that is obtained in the selection step 2, through being carried out curve fitting, data obtain a curve, draw the value of other any times by the curve calculation after the match; Can merge the data that each sensor records with registration this moment by certain criterion.
Embodiment two: present embodiment is described in conjunction with Fig. 1, Fig. 2 and Fig. 3, present embodiment and embodiment one difference are that curve fitting is the spline-fitting of adopting based on least square method in the step 3, splines comes down to a kind of polynomial function piecemeal, if first sensor A is at a certain observed samples time period [a, b] in to target carried out n+1 time the measurement, whole observed samples time interval is divided into by sampling instant: a=t 0<t 1<...<t n=b, given moment point t iCorresponding observed reading is: f (t i)=yi (i=0,1 ..., n), construct a cubic spline functions s (x), and make it satisfy following condition: s (t i)=y i, i=0,1 ..., n; S (t) is at each minizone [t i, t i+ 1] on a cubic polynomial, i=0,1 ..., n-1; S (t) has the Second Order Continuous derivative on [a, b];
It is as follows to make cubic spline functions s (x) satisfy the step of above-mentioned condition:
Splines match based on least square is in the splines space S KIn (Δ), at first find out the optimal approximation about norm ‖ ù ‖, promptly find S for f (t) *(t), make
| | f - S * | | = min S ∈ S k ( Δ ) | | f - s | | - - - ( 1 )
Next constructs cubic spline functions:
Note m i=S ' (t i) (i=0,1,2 ..., n), at each minizone [t i, t i+ 1] (i=0,1,2 ..., n-1) on, utilize the Hermite interpolation formula to write out the computing formula of cubic spline functions s (t):
s ( t ) = ( 1 + 2 t - t i t i + 1 - t i ) ( t - t i + 1 t i - t i + 1 ) 2 y i + ( 1 + 2 t - t i + 1 t i - t i + 1 ) ( t - t i t i + 1 - t i ) 2 y i + 1 + - - - ( 2 )
( t - t i + 1 ) ( t - t i + 1 t i - t i + 1 ) m i ( t - t i + 1 ) ( t - t i t i + 1 - t i ) 2 m i + 1
Utilize s (t) on [a, b], to have the Second Order Continuous derivative; Then s ′ ′ ( t i - ) = s ′ ′ ( t i + ) , (i=0,1,2 ..., n-1), and additional boundary condition S " (t 0)=S " (t n)=0 can get system of equations:
2 m 0 + a 0 m 1 = β 0 ( 1 - a i ) m i - 1 + 2 m i + a i m i + 1 = β i , ( i = 0,1,2 , . . . , n - 1 ) ( 1 - a n ) m n - 1 + 2 m n = β n - - - ( 3 )
Wherein: a 0=1, a i = h i - 1 h i - 1 + h i , i=(1,2,...n-1),a n=0,
β n = 3 h n - 1 ( y n - y n - 1 ) ,
β 0 = 3 h 0 ( y 1 - y 0 ) , β i = 3 ( 1 - a i h i - 1 ( y i - y i - 1 ) + a i h i ( y i + 1 - y i ) ) , ( i = 1,2 , . . . , n - 1 ) ,
h i=t i+1-t i,(i=1,2,...n-1);
2 m 0 + a 0 m 1 = β 0 ( 1 - a 1 ) m 0 + 2 m 1 + a 1 m 2 = β 1 ( 1 - a 2 ) m 1 + 2 m 2 + a 2 m 3 = β 2 . . . . . . . ( 1 - a n - 1 ) m n - 2 + 2 m n - 1 + a n - 1 m n = β n - 1 ( 1 - a n ) m n - 1 + 2 m n + a n m n + 1 = β n , ( i = 0,1,2 , . . . , n - 1 ) - - - ( 4 )
The system of equations matrix of coefficients is a triangular matrix, and its determinant is not 0, so solution of equations exists and be unique; System of equations is found the solution, can be drawn recursion formula:
m i=α im i+1+b i(i=n,n-1,...1,0) (5)
Wherein:
α i = - a i 2 + ( 1 - a i ) a i - 1 , b i = β i - ( 1 - a i ) b i - 1 2 + ( 1 - a i ) a i - 1 , ( i = 0,1,2 , . . . , n - 1 )
α 0 = a 0 2 , b 0 = β 0 2
Using formula is asked α i, b i(i=0,1,2 ..., n-1), make m I+1=0, obtain m nAnd m N-1... m 0, with the parametric t of being given i, y i, m i(i=0,1,2 ..., n-1) substitution s (x) promptly obtains the cubic spline functions asked; Through the spline interpolation match, can obtain a smooth curve, can be by this curve in the hope of first sensor A value at any time.At this moment again and through system to the time the second sensor B carry out time alignment, can take out the measured value in the corresponding moment from this curve according to the sampling instant of the second sensor B, can merge aligning.Other step is identical with embodiment one.

Claims (2)

1, the time unifying method that is used for single or double base complex high-frequency radar nets is characterized in that its step is as follows:
Step 1: set simulation parameter; (T) sets up rectangular coordinate system as true origin with first base station, and the distance of establishing first base station (T) and second base station (R) is L, set moving target (P) again, and to establish moving target (P) initial position be P (L, L), moving target (P) moves horizontally with the straight line that the speed of vm/s is parallel to first base station (T) and place, second base station (R); First sensor (A) in first base station (T) is that collection period comes image data with x second, and second sensor (B) of second base station (R) is that collection period comes image data with y second;
Step 2: carry out emulation according to the simulation parameter in the step 1, and establish first sensor (A) and second sensor (B) when beginning emulation image data, passed through system to the time; In time, first sensor (A) and second sensor (B) collect one group of sampled data based on the described observed samples time in after this one section observed samples;
Step 3: the measurement data of one or two sensor that is obtained in the selection step 2, through being carried out curve fitting, data obtain a curve, draw the value of other any times by the curve calculation after the match.
2, the time unifying method that is used for single or double base complex high-frequency radar nets according to claim 1 is characterized in that curve fitting is the spline-fitting of adopting based on least square method in the step 3; Splines match based on least square is in the splines space S KIn (Δ), at first find out for f (t) about norm || ǜ || optimal approximation, promptly find S *(t), make
| | f - S * | | = min S ∈ S k ( Δ ) | | f - s | | - - - ( 1 )
Next constructs cubic spline functions:
Note m i=S ' (t i) (i=0,1,2 ..., n), at each minizone [t i, t i+ 1] (i=0,1,2 ..., n-1) on, utilize the Hermite interpolation formula to write out the computing formula of cubic spline functions s (t):
s ( t ) = ( 1 + 2 t - t i t i + 1 - t i ) ( t - t i + 1 t i - t i + 1 ) 2 y i + ( 1 + 2 t - t i + 1 t i - t i + 1 ) ( t - t i t i + 1 - t i ) 2 y i + 1 +
(2)
( t - t i + 1 ) ( t - t i + 1 t i - t i + 1 ) m i ( t - t i + 1 ) ( t - t i t i + 1 - t i ) 2 m i + 1
Utilize s (t) on [a, b], to have the Second Order Continuous derivative; Then s ′ ′ ( t i - ) = s ′ ′ ( t i + ) , (i=0,1,2 ..., n-1), and additional boundary condition S " (t 0)=S " (t n)=0 can get system of equations:
2 m 0 + a 0 m 1 = β 0 ( 1 - a i ) m i - 1 + 2 m i + a i m i + 1 = β i ( i = 0,1,2 , · · · , n - 1 ) - - - ( 3 ) ( 1 - a n ) m n - 1 + 2 m n = β n
Wherein: a 0=1, a i = h i - 1 h i - 1 + h i , i=(1,2,...n-1),a n=0,
β 0 = 3 h 0 ( y 1 - y 0 ) , β i = 3 ( 1 - a i h i - 1 ( y i - y i - 1 ) + a i h i ( y i + 1 - y i ) ) (i=1,2,...,n-1), β n = 3 h n - 1 ( y n - y n - 1 ) , h i=t i+1-t i,(i=1,2,...n-1);
2 m 0 + a 0 m 1 = β 0 ( 1 - a 1 ) m 0 + 2 m 1 + a 1 m 2 = β 1 ( 1 - a 2 ) m 1 + 2 m 2 + a 2 m 3 = β 2 · · · · · · · ( 1 - a n - 1 ) m n - 2 + 2 m n - 1 + a n - 1 m n = β n - 1 ( 1 - a n ) m n - 1 + 2 m n + a n m n + 1 = β n , ( i = 0,1,2 , · · · , n - 1 ) - - - ( 4 )
The system of equations matrix of coefficients is a triangular matrix, and its determinant is not 0, so solution of equations exists and be unique;
System of equations is found the solution, can be drawn recursion formula:
m i=α im i+1+b i(i=n,n-1,...1,0) (5)
Wherein:
α i = - a i 2 + ( 1 - a i ) a i - 1 , b i = β i - ( 1 - a i ) b i- 1 2 + ( 1 - a i ) a i - 1 (i=0,1,2,...,n-1)
α 0 = a 0 2 , b 0 = β 0 2
Using formula is asked α i, b i(i=0,1,2 ..., n-1), make m I+1=0, obtain m nAnd m N-1... m 0, with the parametric t of being given i, y i, m i(i=0,1,2 ..., n-1) substitution s (x) promptly obtains the cubic spline functions asked; Through the spline interpolation match, can obtain a smooth curve, can be by this curve in the hope of first sensor (A) value at any time.At this moment again and through system to the time second sensor (B) carry out time alignment, can take out the measured value in the corresponding moment from this curve according to the sampling instant of second sensor (B), can merge aligning.
CN2009100723438A 2009-06-22 2009-06-22 Time alignment method used for single or double base complex high-frequency radar nets Expired - Fee Related CN101598789B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009100723438A CN101598789B (en) 2009-06-22 2009-06-22 Time alignment method used for single or double base complex high-frequency radar nets

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009100723438A CN101598789B (en) 2009-06-22 2009-06-22 Time alignment method used for single or double base complex high-frequency radar nets

Publications (2)

Publication Number Publication Date
CN101598789A true CN101598789A (en) 2009-12-09
CN101598789B CN101598789B (en) 2011-08-10

Family

ID=41420293

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009100723438A Expired - Fee Related CN101598789B (en) 2009-06-22 2009-06-22 Time alignment method used for single or double base complex high-frequency radar nets

Country Status (1)

Country Link
CN (1) CN101598789B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103105601A (en) * 2013-01-07 2013-05-15 哈尔滨工业大学 Maximum posterior principle radiation source position method based on grid search
CN103323840A (en) * 2012-03-22 2013-09-25 中国科学院电子学研究所 Method for time alignment between interference SAR echo data and platform motion and gesture data
CN104683445A (en) * 2015-01-26 2015-06-03 北京邮电大学 Distributed real-time data fusion system
CN105224778A (en) * 2014-06-09 2016-01-06 上海机电工程研究所 General killing area computing method and general launch site computing method

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103323840A (en) * 2012-03-22 2013-09-25 中国科学院电子学研究所 Method for time alignment between interference SAR echo data and platform motion and gesture data
CN103323840B (en) * 2012-03-22 2015-02-11 中国科学院电子学研究所 Method for time alignment between interference SAR echo data and platform motion and gesture data
CN103105601A (en) * 2013-01-07 2013-05-15 哈尔滨工业大学 Maximum posterior principle radiation source position method based on grid search
CN105224778A (en) * 2014-06-09 2016-01-06 上海机电工程研究所 General killing area computing method and general launch site computing method
CN104683445A (en) * 2015-01-26 2015-06-03 北京邮电大学 Distributed real-time data fusion system

Also Published As

Publication number Publication date
CN101598789B (en) 2011-08-10

Similar Documents

Publication Publication Date Title
CN102129063B (en) Method for positioning micro seismic source or acoustic emission source
CN106407677B (en) A kind of multi-object tracking method in the case of missing measurement
CN102435980B (en) Analytical solution-based acoustic emission source or micro seismic source positioning method
CN104809326B (en) A kind of asynchronous sensor spatial registration algorithm
EP2062067B1 (en) Method of and device for tracking an object
CN101598789B (en) Time alignment method used for single or double base complex high-frequency radar nets
CN106093951B (en) Object tracking methods based on array of ultrasonic sensors
CN103728598B (en) The method of track spoofing interference is suppressed with the active radar and passive radar net of other place configure
CN104021292B (en) Dim target detection and tracking method based on formation active networking
CN104808173B (en) Hough transformation-based false point elimination method for direction-finding cross location system
EP2544021A1 (en) Fast ray trace to identify radar multipaths
CN105549005A (en) Dynamic target direction of arrive tracking method based on mesh dividing
CN107526085B (en) Ultrasonic array ranging modeling method and system
CN104715154A (en) Nuclear K-mean value track correlation method based on KMDL criteria
CN103792515B (en) A kind of different platform 2 ties up radar and infrared sensor metric data synthetic method
JPH10142325A (en) Method and system for tracking multiple targets
CN106969767B (en) Estimation method for system deviation of moving platform sensor
CN105319551A (en) Object detection apparatus and method
CN106646482A (en) Transmission line distance detection method, device and system
CN104950300A (en) TOA (time of arrival) range error correcting method and system based on visibility and non-visibility range judgement
CN110471029B (en) Single-station passive positioning method and device based on extended Kalman filtering
CN104075710B (en) A kind of motor-driven Extended target based on Trajectory Prediction axial attitude real-time estimation method
CN105974403B (en) Broad sense divides group's detection method
CN109781116B (en) Error self-calibration fusion positioning method based on active sensor mean value iteration
CN108169722A (en) A kind of unknown disturbances influence the system deviation method for registering of lower sensor

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20110810

Termination date: 20120622