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CN106970361A - The method of estimation of Dual-polarized single pulse radar target angle under disturbed condition - Google Patents

The method of estimation of Dual-polarized single pulse radar target angle under disturbed condition Download PDF

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CN106970361A
CN106970361A CN201710390732.XA CN201710390732A CN106970361A CN 106970361 A CN106970361 A CN 106970361A CN 201710390732 A CN201710390732 A CN 201710390732A CN 106970361 A CN106970361 A CN 106970361A
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polarization
signal
interference
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target
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CN106970361B (en
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王建路
戴幻尧
孔德培
许雄
周波
乔会东
刘文钊
张杨
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UNIT 63892 OF PLA
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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
    • G01S7/36Means for anti-jamming, e.g. ECCM, i.e. electronic counter-counter measures
    • 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
    • G01S13/00Systems 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
    • G01S13/88Radar or analogous systems specially adapted for specific applications

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  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
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  • Radar Systems Or Details Thereof (AREA)

Abstract

The method of estimation of Dual-polarized single pulse radar target angle under disturbed condition, it is related to Radar ECM technical field, radar receiving antenna is changed to the reception of double polarization, and increase corresponding sum-difference network, receiving channel, form Dual-polarized single pulse radar, according to radar horizon polarize three passages and, gun parallax, trim output data, three passages of vertical polarization and, gun parallax, trim output data, estimate the polarization characteristic of composite interference, the polarization ratio of interference is brought into mathematical formulae to solve, eliminate coupling error of the interference signal to angle on target, estimate the real angle of target;It is simple and effective that the present invention provides one kind for confrontation main lobe composite interference, and is highly susceptible to the method for Project Realization;Present invention could apply in existing target radar, track and guidance radar, end-guidance radar, fire control radar, with important reality.

Description

The method of estimation of Dual-polarized single pulse radar target angle under disturbed condition
Technical field
The present invention relates to Radar ECM technical field, more particularly, to Dual-polarized single pulse radar mesh under disturbed condition Mark the method for estimation of angle.
Background technology
Known, monopulse radar angle measurement has been a kind of technology of relative maturity and has been widely used in high-precision tracking thunder Up in system.However, when there is the close and different target of angle and noise jamming source simultaneously in radar main beam, mesh Mark echo is flooded in time domain and frequency domain by the interference with certain bandwidth, and after conventional signal transacting, monopulse radar can not Effective detection target, or mistake detection, tracking source, Monopulse estimation be output as physical space target and interference plus Weight average, it is impossible to provide correct angle and indicate, and then destroy radar angular tracking system.When this major lobe suppression not only has The interference effect of frequency domain compacting, it may have the interference effect of angle deception, we term it main lobe composite interference.For example, active Radar decoy interference (towed radar active decoy, TRAD) is generally bigger than the amplitude of real goal echo-signal very It is many, relation spatially is maintained a certain distance with target, target and bait interference can not be differentiated in the range of radar main beam, Bait can be suppressed with Turnaround Noise and disturbed, and greatly destroy monopulse radar to the accurate of the angle measurement of real goal and tracking Degree.
At present, monopulse radar has several counterchecks to conventional major lobe suppression, but does not have to composite interference in main lobe There is good anti-interference method.Existing radar resists general major lobe suppression can be with:(1) radar transmission power is improved, takes and " burns Wear pattern ", electronic interferences is failed on certain distance.Burn-through range is proportional to the RCS of target fourth root, typically goes out Present to be immediated vicinity from radar, this causes radar long-term work in disturbed state.(2) Range resolution of radar is improved Power, using the transmitted signal bandwidth of more than 100M radar, makes the high resolution range power of radar reach the rank of rice, it is intended to from away from Target and interference source are differentiated from.This method is that a Single Point Source interference effect is relatively good to interference source in main lobe, But be otiose to main lobe composite interference.Because main lobe composite interference is entirely being covered with target time in range Ripple, rather than the only range cell coverage goal echo where target, even if improving resolving power, other resolution cells it is dry Disturb signal still to exist, so that can not be apart from upper resolution target and interference;(3) radar angular resolving power is improved, using space Power estimation technology, makes radar angular resolving power reach the 1/2 of beam angle, and target and interference source are differentiated in angle. But actually spatial spectral estimation algorithm requires very high to signal to noise ratio, operand is very big, is difficult to realize in engineering, composite interference In noise jamming composition after can raise noise of radar receiver level, reduce signal to noise ratio so that the property of Estimation of Spatial Spectrum technology It can be greatly lowered.(4) direct polarization filtering means are used, polarization filtering is carried out with passage, poor passage respectively pair and suppresses interference Signal, then filtered signal is subjected to Monopulse estimation processing.But it is due to the presence of residual interference signal after filtering so that Angular metric measured value is constantly present certain deviation, in addition, filtering is possible to that signal to noise ratio can be reduced, follow-up detection band is disappeared Pole influences.
The content of the invention
In order to overcome the shortcomings of in background technology, the invention discloses Dual-polarized single pulse radar target angle under disturbed condition The method of estimation of degree.
In order to realize the goal of the invention, the present invention is adopted the following technical scheme that:
The method of estimation of Dual-polarized single pulse radar target angle, specifically includes following steps under disturbed condition:
(1) monopulse radar, is changed to single polarization transmitting, reception of double polarization working method:
The reception of double polarization working method is all dual-polarized per exporting all the way for four quadrants of antenna, per defeated all the way Go out including horizontal polarization and vertical polarization two-way, each quadrant has two-way output, four quadrants have 8 tunnel output signals, specifically For:
The vertical polarization output A on A roadsv, horizontal polarization output Ah
The vertical polarization output B on B roadsv, horizontal polarization output Bh
The vertical polarization output C on C roadsv, horizontal polarization output Ch
The vertical polarization output D on D roadsv, horizontal polarization output Dh
8 tunnel output signals of aforementioned four quadrant are subjected to linear combinations, constitute six roads and, difference signal, including:Level pole Change and signal Σh, horizontal polarization gun parallax signal deltah,A, horizontal polarization trim signal deltah,E, the sum of vertical polarization Signal Σv, vertical polarization gun parallax signal deltav,A, vertical polarization trim signal deltav,E
Above-mentioned six road and, the relation of 8 tunnel output signals of difference signal and A, B, C, D four-quadrant, be expressed as follows:
Σv=Av+Bv+Cv+Dv
Σh=Ah+Bh+Ch+Dh
Δv,A=(Av+Cv)-(Bv+Dv)
Δv,E=(Av+Bv)-(Cv+Dv)
Σh,A=(Ah+Ch)-(Bh+Dh)
Δh,E=(Ah+Bh)-(Ch+Dh)
(2), basis and the output signal of passage, calculate the polarization ratio of composite interference signal:
In the range of radar main beam, while when there is the different target of angle and interference source, and passage output signal Echo signal and interference signal are contained, therefore, the signal of vertical polarization and passage, horizontal polarization and passage is as follows:
ΣvTvIv
ΣhThIh
Because interfering signal power is strong, echo signal is disturbed signal and flooded, and interference and echo signal power ratio disturb letter Number power is more than 15dB, i.e. ΣTV<<ΣIV, ΣTh<<ΣIh, therefore main the hanging down with interference signal of output of vertical polarization passage Based on straight polarization components, the output of horizontal polarization passage is main based on the horizontal polarized components of interference signal:
Σv≈ΣIv
Σh≈ΣIh
The polarization characteristic of interference signal is polarization ratio, with horizontal polarization and passage, vertical polarization and passage export number According to Σh(t),Σv(t), obtain:
According to above-mentioned formula, the polarization ratio of interference signal carries out polarization using the echo-signal in the two POLARIZATION CHANNELs and estimated Meter is obtained, and then the polarization ratio estimate result to different distance/frequency cells takes average;
(3) pre-processed with passage polarization filtering, distance/speed resolution cell of search target and interference aliasing:
The interference polarization vector estimated according to step (2) is [cos γ sin γ e]T, based on rectangular projection criterion, if AF panel polarisation filter is counted, filter vector H is met
H=[sin γ cos γ e-jφ]T
There are two and passage (Σ of target echo signal and interference signal to aliasingvh) polarization filtering is carried out, obtain one Individual pretreated and signal ΣPF
Two and passage after filtering after, interference signal is suppressed significantly, and is detected according to filtered data, is searched for Distance/speed resolution cell where target and interference aliasing is found, and the distance/speed resolution cell is labeled as Ω, and By 6 tunnel primary signals where the Ω units, non-filtered treated signal extraction comes out, and obtains horizontal polarization and vertical pole Change passage is exported and signal Σv(Ω),ΣhThe gun parallax signal delta of (Ω), horizontal polarization and the output of vertical polarization passagev,A (Ω),Δh,AThe trim signal delta of (Ω), horizontal polarization and the output of vertical polarization passagev,E(Ω),Δh,E(Ω);
(4) angular estimation method is decoupled using dual polarization:
Distance/speed resolution cell of aliasing is occurred according to target and interference, by two-way and signal Σv(Ω),Σh(Ω), The gun parallax signal delta of horizontal polarization and vertical polarizationv,A(Ω),Δh,A(Ω), and interference polarization substitute into following public affairs than p Formula, it is possible to remove the angle measurement deviation that interference is introduced, the azimuth angle theta of real goal is directly estimated under interference environmentT,A
(5), exported according to horizontal polarization and vertical polarization passage and signal Σv(Ω),Σh(Ω), horizontal polarization and hang down The trim signal delta directly polarizedv,Eh,E, and interference polarization is than p, the following formula of substitution, it is possible to remove interference and introduce Angle measurement deviation, the angle of pitch of real goal is directly estimated under interference environment:
Subscript v tables in the method for estimation of Dual-polarized single pulse radar target angle under described disturbed condition, step (1) Show vertical polarization, h represents horizontal polarization, and A represents azimuth, and E represents the angle of pitch..
Subscript, T in the method for estimation of Dual-polarized single pulse radar target angle under described disturbed condition, step (2) Target is represented, I represents interference, ΣTvRepresent the perpendicular polarisation components of target, ΣIvRepresent the perpendicular polarisation components of interference signal. ΣThRepresent the horizontal polarized components of target, ΣIhRepresent the horizontal polarized components of interference signal.
T is in formula in the method for estimation of Dual-polarized single pulse radar target angle under described disturbed condition, step (2) Time/frequency mark, different t represents different distance/speed units,.
K is pulse in the method for estimation of Dual-polarized single pulse radar target angle under described disturbed condition, step (4) The angle of radar differentiates the slope of curve, is known quantity.Subscript A represents azimuth.
K is pulse in the method for estimation of Dual-polarized single pulse radar target angle under described disturbed condition, step (5) The angle of radar differentiates the slope of curve, is known quantity;Footmark E represents the angle of pitch.
By adopting the above-described technical solution, the present invention has the advantages that:
1st, under disturbed condition of the present invention Dual-polarized single pulse radar target angle method of estimation, by radar antenna Dual polarized antenna is improved to by single-polarized antenna, Monopulse radar receiver is improved, increases sum-difference network, horizontal polarization three is extracted Individual multi-channel output signal, three multi-channel output signals of vertical polarization, combining target, the polarization characteristic measurement of interference, solve mathematics Equation, eliminates interference signal to the coupling error of angle on target, estimates the real angle of target, for confrontation main lobe composite interference It is simple and effective there is provided one kind, and it is highly susceptible to the method for Project Realization;Present invention could apply to existing Target indication thunder Reach, in track and guidance radar, end-guidance radar, fire control radar, have important practical significance.
2nd, conventional single-pulse radar antenna is generally vertical polarization or horizontal polarization, and transmitting and the signal received are list One polarized signal;In practice, target echo and the existing perpendicular polarisation components of main lobe composite interference signal, there is horizontal polarization point again Amount, single polarization transmitting is changed to by radar, and reception of double polarization working method can receive the horizontal polarized components of echo-signal simultaneously And perpendicular polarisation components.
Brief description of the drawings
Fig. 1 is that the Dual-polarized single pulse radar antenna four-quadrant after the present invention is improved constitutes schematic diagram;
Fig. 2 is the Dual-polarized single pulse radar receiver system composition structure chart after the present invention is improved;
Fig. 3 is Dual-polarized single pulse radar target angle measurement procedure figure under main lobe composite interference;
Fig. 4 is the time domain distribution of monopulse radar and passage (H+V) reception signal under main lobe composite interference;
Fig. 5 is the frequency domain distribution of monopulse radar and passage (H+V) reception signal under the conditions of main lobe composite interference;
Fig. 6 is the testing result of the Range resolution unit of target and interference aliasing after being pre-processed with passage polarization filtering;
Fig. 7 is the testing result of the speed resolution cell of target and interference aliasing after being pre-processed with passage polarization filtering;
Fig. 8 is the real angle where target and interference source;
Fig. 9 is conventional single-pulse radar target angle estimated result under the conditions of main lobe composite interference;
Figure 10 is Dual-polarized single pulse radar target angle estimated result (representative value ISR=under the conditions of main lobe composite interference 20dB, 15dB);
Figure 11 estimates performance with receiver noise for Dual-polarized single pulse radar target angle under the conditions of main lobe composite interference The change of coefficient;
Figure 12 is (polarization ratio evaluated error) Dual-polarized single pulse radar target angle under different polarization estimate deflection conditions Estimate performance.
Embodiment
Explanation that can be detailed by the following examples is of the invention, and the open purpose of the present invention is intended to protect model of the present invention Enclose all interior technological improvements.
With reference to the method for estimation of Dual-polarized single pulse radar target angle under accompanying drawing 1-12 disturbed conditions, specifically include following Step:
(1) monopulse radar, is changed to single polarization transmitting, reception of double polarization working method:
Radar receiving antenna is changed to the reception of double polarization and increases corresponding sum-difference network, receiving channel, dual polarization is formed Monopulse radar, the reception of double polarization working method for antenna four quadrants per export all the way be all it is dual-polarized, it is each Road output includes horizontal polarization and vertical polarization two-way, and each quadrant has two-way output, and four quadrants have 8 tunnel output signals, Specially:
The vertical polarization output A on A roadsv, horizontal polarization output Ah
The vertical polarization output B on B roadsv, horizontal polarization output Bh
The vertical polarization output C on C roadsv, horizontal polarization output Ch
The vertical polarization output D on D roadsv, horizontal polarization output Dh
8 tunnel output signals of aforementioned four quadrant are subjected to linear combinations, constitute six roads and, difference signal, including:Level pole Change and signal Σh, horizontal polarization gun parallax signal deltah,A, horizontal polarization trim signal deltah,E, the sum of vertical polarization Signal Σv, vertical polarization gun parallax signal deltav,A, vertical polarization trim signal deltav,E
Above-mentioned six road and, the relation of 8 tunnel output signals of difference signal and A, B, C, D four-quadrant, be expressed as follows:
Σv=Av+Bv+Cv+Dv
Σh=Ah+Bh+Ch+Dh
Δv,A=(Av+Cv)-(Bv+Dv)
Δv,E=(Av+Bv)-(Cv+Dv)
Σh,A=(Ah+Ch)-(Bh+Dh)
Δh,E=(Ah+Bh)-(Ch+Dh)
(2), basis and the output signal of passage, calculate the polarization ratio of composite interference signal:
In the range of radar main beam, while when there is the different target of angle and interference source, and passage output signal Echo signal and interference signal are contained, therefore, the signal of vertical polarization and passage, horizontal polarization and passage is as follows:
ΣvTvIv
ΣhThIh
Because interfering signal power is strong, echo signal is disturbed signal and flooded, and interference and echo signal power ratio disturb letter Number power is more than 15dB, i.e. ΣTV<<ΣIV, ΣTh<<ΣIh, therefore main the hanging down with interference signal of output of vertical polarization passage Based on straight polarization components, the output of horizontal polarization passage is main based on the horizontal polarized components of interference signal:
Σv≈ΣIv
Σh≈ΣIh
The polarization characteristic of interference signal is polarization ratio, with horizontal polarization and passage, vertical polarization and passage export number According to Σh(t),Σv(t), obtain:
According to above-mentioned formula, the polarization ratio of interference signal carries out polarization using the echo-signal in the two POLARIZATION CHANNELs and estimated Meter is obtained, and then the polarization ratio estimate result to different distance/frequency cells takes average;
(3) pre-processed with passage polarization filtering, distance/speed resolution cell of search target and interference aliasing:
The interference polarization vector estimated according to step (2) is [cos γ sin γ e]T, based on rectangular projection criterion, if AF panel polarisation filter is counted, filter vector H is met
H=[sin γ cos γ e-jφ]T
There are two and passage (Σ of target echo signal and interference signal to aliasingvh) polarization filtering is carried out, obtain one Individual pretreated and signal ΣPF
Two and passage after filtering after, interference signal is suppressed significantly, and is detected according to filtered data, is searched for Distance/speed resolution cell where target and interference aliasing is found, and the distance/speed resolution cell is labeled as Ω, and By 6 tunnel primary signals where the Ω units, non-filtered treated signal extraction comes out, and obtains horizontal polarization and vertical pole Change passage is exported and signal Σv(Ω),ΣhThe gun parallax signal delta of (Ω), horizontal polarization and the output of vertical polarization passagev,A (Ω),Δh,AThe trim signal delta of (Ω), horizontal polarization and the output of vertical polarization passagev,E(Ω),Δh,E(Ω);
(4) angular estimation method is decoupled using dual polarization:
Distance/speed resolution cell of aliasing is occurred according to target and interference, by two-way and signal Σv(Ω),Σh(Ω), The gun parallax signal delta of horizontal polarization and vertical polarizationv,A(Ω),Δh,A(Ω), and interference polarization substitute into following public affairs than p Formula, it is possible to remove the angle measurement deviation that interference is introduced, the azimuth angle theta of real goal is directly estimated under interference environmentT,A
(5), exported according to horizontal polarization and vertical polarization passage and signal Σv(Ω),Σh(Ω), horizontal polarization and hang down The trim signal delta directly polarizedv,Eh,E, and interference polarization is than p, the following formula of substitution, it is possible to remove interference and introduce Angle measurement deviation, the angle of pitch of real goal is directly estimated under interference environment:
Subscript v tables in the method for estimation of Dual-polarized single pulse radar target angle under described disturbed condition, step (1) Show vertical polarization, h represents horizontal polarization, and A represents azimuth, and E represents the angle of pitch..
Subscript, T in the method for estimation of Dual-polarized single pulse radar target angle under described disturbed condition, step (2) Target is represented, I represents interference, ΣTvRepresent the perpendicular polarisation components of target, ΣIvRepresent the perpendicular polarisation components of interference signal. ΣThRepresent the horizontal polarized components of target, ΣIhRepresent the horizontal polarized components of interference signal.
T is in formula in the method for estimation of Dual-polarized single pulse radar target angle under described disturbed condition, step (2) Time/frequency mark, different t represents different distance/speed units,.
K is pulse in the method for estimation of Dual-polarized single pulse radar target angle under described disturbed condition, step (4) The angle of radar differentiates the slope of curve, is known quantity.Subscript A represents azimuth.
K is pulse in the method for estimation of Dual-polarized single pulse radar target angle under described disturbed condition, step (5) The angle of radar differentiates the slope of curve, is known quantity;Footmark E represents the angle of pitch.
Implement the method for estimation of Dual-polarized single pulse radar target angle under disturbed condition of the present invention, Fig. 1 is this Dual-polarized single pulse radar antenna four-quadrant after invention is improved constitutes schematic diagram.Whole antenna is flat board gap array, is had Tetra- quadrants of A, B, C, D are constituted, and the antenna element of each quadrant is dual-polarized, including horizontal polarization and vertical polarization two-way. Horizontal polarization is operated in during the antenna transmission signal, horizontal polarization echo and vertical polarization echo can be received during reception simultaneously.
Fig. 2 is the Dual-polarized single pulse radar receiver system composition structure chart after the present invention is improved.
It can be seen that, each quadrant has the output of two-way polarized signal, and four quadrants just have 8 tunnel output signals:
The vertical polarization output A on A roadsv, horizontal polarization output Ah
The vertical polarization output B on B roadsv, horizontal polarization output Bh
The vertical polarization output C on C roadsv, horizontal polarization output Ch
The vertical polarization output D on D roadsv, horizontal polarization output Dh
This 8 tunnel output signal is carried out by two sum-difference networks (horizontal polarization sum-difference network, vertical polarization sum-difference network) Linear combination, may be constructed six road signals, including:Horizontal polarization and signal Σh, horizontal polarization gun parallax signal deltah,A、 The trim signal delta of horizontal polarizationh,E, vertical polarization and signal Σv, vertical polarization gun parallax signal deltav,A, vertical pole The trim signal delta of changev,E.Subscript v represents vertical polarization, and h represents horizontal polarization, and A represents azimuth, and E represents the angle of pitch.
Fig. 3 is Dual-polarized single pulse radar target angle measurement procedure figure under main lobe composite interference.According to two and poor net The horizontal polarization and channel signal and vertical polarization and signal of network output, calculate the polarization ratio of composite interference signal, calculate Polarization filtering vector, is pre-processed, interference signal can be significantly inhibited after filtering, greatly to the conscientious polarization filtering of two-way and passage Amplitude improves signal interference ratio, finds the distance/speed resolution cell at the place of target and interference aliasing, determines after the unit, to six The distance of road signal/speed resolution cell decouples angular estimation method using dual polarization, estimates the orientation and the angle of pitch of target.
Fig. 4 is the time domain distribution that monopulse radar and passage (H+V) receive signal under main lobe composite interference, now interference and Echo signal power ratio is 15dB, and because jam-to-signal echo signal is big 15 decibels, now echo signal is pressed completely, Echo signal can not be detected in time domain.
Fig. 5 is the frequency domain distribution of monopulse radar and passage (H+V) reception signal under the conditions of main lobe composite interference.Now do It is 15dB to disturb with echo signal power ratio, and because jam-to-signal echo signal is big 15 decibels, the frequency spectrum of interference signal covers completely Frequency where lid target, now echo signal be pressed completely, echo signal can not be detected in frequency domain.
Fig. 6, Fig. 7 are the inspections of distance/speed resolution cell of target and interference aliasing after being pre-processed with passage polarization filtering Survey result.It can be seen that, and signal and noise power ratio are greatly improved after passage polarization filtering pretreatment, can be substantially The general residing distance of target and speed resolution cell are told, is found out from figure, target is approximately at 0.1 × 10-3Position when On the position of domain, the unit is found in 0.2KHz frequency location, automatic search, for next step processing.
Fig. 8 gives the actual position where target and interference, and the orientation and the angle of pitch of target are all -1 degree, the side of interference Position and the angle of pitch are 1.5 degree, and beam angle is 6 degree.
Fig. 9 is conventional single-pulse radar target angle estimated result under the conditions of main lobe composite interference.In main lobe composite interference Under, interference signal causes radar angle measurement to produce very big error, because interfering signal power is stronger than echo signal power 20 decibels, this When conventional single-pulse processing angle measurement output it is most of be interference signal angle, so the orientation and the angle of pitch of angle measurement output are general In 1.5 degree, 1.5 degree of scopes.
Figure 10 is Dual-polarized single pulse radar target angle estimated result under the conditions of main lobe composite interference, now interference signal Power ratio ISR=20dB, radio-frequency channel itself signal to noise ratio snr=20dB, it can be seen that according to the New Method for Processing of patent can be with The angle where target is more accurately estimated under disturbed condition.
Figure 11 estimates performance with receiver noise for Dual-polarized single pulse radar target angle under the conditions of main lobe composite interference The change of coefficient.It can be seen that, signal to noise ratio is higher, and the estimation performance of new method is better, it is meant that receiver signal to noise ratio itself is got over Height, noise coefficient is lower, and the angle estimation performance of radar target is higher.
Figure 12 is Dual-polarized single pulse radar target angle estimation performance under different polarization estimate deflection conditions.Assuming that interference Polarization ratio evaluated error between 0-0.2, phase estimation error be 15 degree, the angular estimation error of radar target is with polarization ratio The increase of evaluated error and increase, this explanation interference polarization estimate error it is smaller, the angle estimation error of radar target is smaller.

Claims (6)

1. the method for estimation of Dual-polarized single pulse radar target angle under disturbed condition, it is characterized in that:Specifically include following steps:
(1) monopulse radar, is changed to single polarization transmitting, reception of double polarization working method:
The reception of double polarization working method is all dual-polarized per exporting all the way for four quadrants of antenna, per output bag all the way Horizontal polarization and vertical polarization two-way are included, each quadrant has two-way output, and four quadrants have 8 tunnel output signals, be specially:
The vertical polarization output A on A roadsv, horizontal polarization output Ah
The vertical polarization output B on B roadsv, horizontal polarization output Bh
The vertical polarization output C on C roadsv, horizontal polarization output Ch
The vertical polarization output D on D roadsv, horizontal polarization output Dh
8 tunnel output signals of aforementioned four quadrant are subjected to linear combinations, constitute six roads and, difference signal, including:Horizontal polarization With signal Σh, horizontal polarization gun parallax signal deltah,A, horizontal polarization trim signal deltah,E, vertical polarization and signal Σv, vertical polarization gun parallax signal deltav,A, vertical polarization trim signal deltav,E
Above-mentioned six road and, the relation of 8 tunnel output signals of difference signal and A, B, C, D four-quadrant, be expressed as follows:
Σv=Av+Bv+Cv+Dv
Σh=Ah+Bh+Ch+Dh
Δv,A=(Av+Cv)-(Bv+Dv)
Δv,E=(Av+Bv)-(Cv+Dv)
Σh,A=(Ah+Ch)-(Bh+Dh)
Δh,E=(Ah+Bh)-(Ch+Dh)
(2), basis and the output signal of passage, calculate the polarization ratio of composite interference signal:
In the range of radar main beam, while when there is the different target of angle and interference source, and the output signal of passage is included Echo signal and interference signal, therefore, the signal of vertical polarization and passage, horizontal polarization and passage is as follows:
ΣvTvIv
ΣhThIh
Because interfering signal power is strong, echo signal is disturbed signal and flooded, interference and echo signal power ratio interference signal work( Rate is more than 15dB, i.e. ΣTV<<ΣIV, ΣTh<<ΣIh, therefore the main vertical pole with interference signal of output of vertical polarization passage Change based on component, the output of horizontal polarization passage is main based on the horizontal polarized components of interference signal:
Σv≈ΣIv
Σh≈ΣIh
The polarization characteristic of interference signal is polarization ratio, with horizontal polarization and passage, vertical polarization and passage output data Σh (t),Σv(t), obtain:
p &ap; &Sigma; h ( t ) &OverBar; &Sigma; v ( t ) ;
According to above-mentioned formula, the polarization ratio of interference signal carries out polarization estimate using the echo-signal in the two POLARIZATION CHANNELs and obtained Arrive, then the polarization ratio estimate result to different distance/frequency cells takes average;(3) pre-processed with passage polarization filtering, Search for distance/speed resolution cell of target and interference aliasing:
The interference polarization vector estimated according to step (2) is [cos γ sin γ e]T, based on rectangular projection criterion, design is dry Suppression polarisation filter is disturbed, filter vector H is met
H=[sin γ cos γ e-jφ]T
There are two and passage (Σ of target echo signal and interference signal to aliasingvh) polarization filtering is carried out, obtain one in advance After processing and signal ΣPF
&Sigma; P F = H T &CenterDot; &Sigma; h &Sigma; v
Two and passage after filtering after, interference signal is suppressed significantly, and is detected that search is found according to filtered data Distance/speed resolution cell where target and interference aliasing, and the distance/speed resolution cell is labeled as Ω, and should 6 tunnel primary signals where Ω units, non-filtered treated signal extraction comes out, and obtains horizontal polarization and vertical polarization is logical Road is exported and signal Σv(Ω),ΣhThe gun parallax signal delta of (Ω), horizontal polarization and the output of vertical polarization passagev,A(Ω), Δh,AThe trim signal delta of (Ω), horizontal polarization and the output of vertical polarization passagev,E(Ω),Δh,E(Ω);
(4) angular estimation method is decoupled using dual polarization:
Distance/speed resolution cell of aliasing is occurred according to target and interference, by two-way and signal Σv(Ω),Σh(Ω), level Polarization and the gun parallax signal delta of vertical polarizationv,A(Ω),Δh,A(Ω), and interference polarization substitute into following formula, just than p The angle measurement deviation that interference is introduced can be removed, the azimuth angle theta of real goal is directly estimated under interference environmentT,A
&theta; T , A = 1 k p&Delta; v , A ( &Omega; ) - &Delta; h , A ( &Omega; ) p&Sigma; v ( &Omega; ) - &Sigma; h ( &Omega; ) ;
(5), exported according to horizontal polarization and vertical polarization passage and signal Σv(Ω),Σh(Ω), horizontal polarization and vertical pole The trim signal delta of changev,Eh,E, and interference polarization is than p, the following formula of substitution, it is possible to remove the survey that interference is introduced Angular displacement, directly estimates the angle of pitch of real goal under interference environment:
&theta; T , E = 1 k p&Delta; v , E ( &Omega; ) - &Delta; h , E ( &Omega; ) p&Sigma; v ( &Omega; ) - &Sigma; h ( &Omega; ) .
2. the method for estimation of Dual-polarized single pulse radar target angle under disturbed condition according to claim 1, its feature It is:Subscript v represents vertical polarization in step (1), and h represents horizontal polarization, and A represents azimuth, and E represents the angle of pitch.
3. the method for estimation of Dual-polarized single pulse radar target angle under disturbed condition according to claim 1, its feature It is:Subscript in step (2), T represents target, and I represents interference, ΣTvRepresent the perpendicular polarisation components of target, ΣIvRepresent interference The perpendicular polarisation components of signal.ΣThRepresent the horizontal polarized components of target, ΣIhRepresent the horizontal polarized components of interference signal.
4. the method for estimation of Dual-polarized single pulse radar target angle under disturbed condition according to claim 1, its feature It is:T is time/frequency mark in formula in step (2), and different t represents different distance/speed units.
5. the method for estimation of Dual-polarized single pulse radar target angle under disturbed condition according to claim 1, its feature It is:K differentiates the slope of curve for the angle of monopulse radar in step (4), is known quantity.Subscript A represents azimuth.
6. the method for estimation of Dual-polarized single pulse radar target angle under disturbed condition according to claim 1, its feature It is:K differentiates the slope of curve for the angle of monopulse radar in step (5), is known quantity;Footmark E represents the angle of pitch.
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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108988928A (en) * 2018-05-23 2018-12-11 中国电子科技集团公司第五十四研究所 A method of the detection of two-channel monopulse angle error is carried out in frequency domain
WO2019155456A1 (en) * 2018-02-12 2019-08-15 Israel Aerospace Industries Ltd. Radar system and method for determining direction to an object
CN110857979A (en) * 2018-08-26 2020-03-03 吴成彬 Coherent signal-based anti-interference identification system and method for polarization frequency selection characteristic material
RU2720588C1 (en) * 2018-11-15 2020-05-12 Игорь Валерьевич Демичев Method and device for spatial selection of electromagnetic waves with subsequent polarization processing of signals
CN111190145A (en) * 2020-03-03 2020-05-22 中国人民解放军63892部队 Arbitrary polarization signal generating device and method
CN111948598A (en) * 2020-07-30 2020-11-17 西南电子技术研究所(中国电子科技集团公司第十研究所) Method and device for detecting space domain interference signal
CN112068119A (en) * 2020-07-28 2020-12-11 中国人民解放军63892部队 Method for recognizing interference of passive radar guide head on radar and bait
RU2743785C1 (en) * 2020-07-13 2021-02-26 Федеральное государственное казенное учреждение "12 Центральный научно-исследовательский институт" Министерства обороны Российской Федерации Method of determining location of a spherical light source by a ground surveillance apparatus
CN113253206A (en) * 2021-04-25 2021-08-13 北京理工大学 Variable polarization monopulse radar target angle estimation method, system, device and medium
CN114675257A (en) * 2022-05-30 2022-06-28 中国人民解放军国防科技大学 A non-rectangular array polarimetric monopulse radar dual target discrimination method
CN116068502A (en) * 2023-04-06 2023-05-05 中国人民解放军空军预警学院 Multi-domain combined anti-composite interference method, device and system
CN117879736A (en) * 2024-03-13 2024-04-12 中国人民解放军海军工程大学 A method and device for measuring shortwave environmental noise based on vector antenna

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102565790A (en) * 2012-01-02 2012-07-11 西安电子科技大学 Self-adaptive sum-difference angle measurement method for plane phased array
CN104166136A (en) * 2014-07-11 2014-11-26 河海大学 Interference subspace tracking-based high-efficiency self-adaptive monopulse angle measurement method
US20160173149A1 (en) * 2013-04-09 2016-06-16 Maxlinear, Inc. Automatic Twist and Sway Compensation in a Microwave Backhaul Transceiver
CN105785340A (en) * 2016-05-23 2016-07-20 中国人民解放军63892部队 Angle-measuring and identifying method for target and bait interferences in main lobe of monopulse radar
CN106125039A (en) * 2016-06-14 2016-11-16 河海大学 Improvement space-time adaptive Monopulse estimation method based on local Combined Treatment

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102565790A (en) * 2012-01-02 2012-07-11 西安电子科技大学 Self-adaptive sum-difference angle measurement method for plane phased array
US20160173149A1 (en) * 2013-04-09 2016-06-16 Maxlinear, Inc. Automatic Twist and Sway Compensation in a Microwave Backhaul Transceiver
CN104166136A (en) * 2014-07-11 2014-11-26 河海大学 Interference subspace tracking-based high-efficiency self-adaptive monopulse angle measurement method
CN105785340A (en) * 2016-05-23 2016-07-20 中国人民解放军63892部队 Angle-measuring and identifying method for target and bait interferences in main lobe of monopulse radar
CN106125039A (en) * 2016-06-14 2016-11-16 河海大学 Improvement space-time adaptive Monopulse estimation method based on local Combined Treatment

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
KEYLAM.MORA-NAVARRO: "POLARIZATION EFFECTS ON A SINGLE POLARIZED OFF-THE-GRID X-BAND RADAR", 《IEEE IGARSS 2013》 *
马佳智等: "主瓣干扰下混合极化系统单脉冲角度估计方法", 《系统工程与电子技术》 *

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019155456A1 (en) * 2018-02-12 2019-08-15 Israel Aerospace Industries Ltd. Radar system and method for determining direction to an object
US11276944B2 (en) 2018-02-12 2022-03-15 Israel Aerospace Industries Ltd. Radar system and method for determining direction to an object
CN108988928A (en) * 2018-05-23 2018-12-11 中国电子科技集团公司第五十四研究所 A method of the detection of two-channel monopulse angle error is carried out in frequency domain
CN108988928B (en) * 2018-05-23 2020-09-22 中国电子科技集团公司第五十四研究所 Method for detecting double-channel single-pulse angle error in frequency domain
CN110857979A (en) * 2018-08-26 2020-03-03 吴成彬 Coherent signal-based anti-interference identification system and method for polarization frequency selection characteristic material
CN110857979B (en) * 2018-08-26 2024-05-14 吴成彬 Anti-interference identification system and method for polarization frequency selection characteristic material based on coherent signal
RU2720588C1 (en) * 2018-11-15 2020-05-12 Игорь Валерьевич Демичев Method and device for spatial selection of electromagnetic waves with subsequent polarization processing of signals
CN111190145A (en) * 2020-03-03 2020-05-22 中国人民解放军63892部队 Arbitrary polarization signal generating device and method
RU2743785C1 (en) * 2020-07-13 2021-02-26 Федеральное государственное казенное учреждение "12 Центральный научно-исследовательский институт" Министерства обороны Российской Федерации Method of determining location of a spherical light source by a ground surveillance apparatus
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CN111948598A (en) * 2020-07-30 2020-11-17 西南电子技术研究所(中国电子科技集团公司第十研究所) Method and device for detecting space domain interference signal
CN113253206A (en) * 2021-04-25 2021-08-13 北京理工大学 Variable polarization monopulse radar target angle estimation method, system, device and medium
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