AU602974B2 - Beamforming/null-steering adaptive array - Google Patents

Beamforming/null-steering adaptive array Download PDF

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Publication number
AU602974B2
AU602974B2 AU14750/88A AU1475088A AU602974B2 AU 602974 B2 AU602974 B2 AU 602974B2 AU 14750/88 A AU14750/88 A AU 14750/88A AU 1475088 A AU1475088 A AU 1475088A AU 602974 B2 AU602974 B2 AU 602974B2
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Australia
Prior art keywords
epoch
signal
output
gate
desired signal
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AU14750/88A
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AU1475088A (en
Inventor
Raymond J. Masak
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BAE Systems Aerospace Inc
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Hazeltine Corp
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Priority claimed from CA000563730A external-priority patent/CA1325260C/en
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/26Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture
    • H01Q3/2605Array of radiating elements provided with a feedback control over the element weights, e.g. adaptive arrays
    • H01Q3/2611Means for null steering; Adaptive interference nulling
    • H01Q3/2617Array of identical elements

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  • Variable-Direction Aerials And Aerial Arrays (AREA)

Description

FORTYORTY DOLLARS TWENTY DOLLARS AUSTRALIA I7 4 PATENTS ACT 1952 Form COMPLETE SPECIFICATION
(ORIGINAL)
FOR OFFICE USE Short Title: Int. Cl: Application Number: Lodged: Complete Specification-Lodged: Accerted: Lapsed: Published: aIa a12 -6 H ~Lrq~U Priority: Related Art: TO BE COMPLETED BY APPLICANT Name of Applicant: Address of Applicant: or .C HAZELTINE CORPORATION
GREENLAWN,
NEW YORK 11740
U.S.A.
Actual Inventor: Address for Service: GRIFFITH HACK CO., 601 St. Kilda Road, Melbourne, Victoria 3004, Australia.
Complete Specification for the invention entitled: BEAMFORMING/NULL-STEERING ADAPTIVE ARRAY The following statement is a full description of this invention including the best method of performing it known to me:- VM A" vo y 1Position Assistant GRIFFITH HACK
CO
PATENT AN D TRADE MARK ATTORNEYS MELBOU R N E SYDNEY
PERTH
1A BEAMFORMING/NULL-STEERING ADAPTIVE ARRAY FIELD OF THE INVENTION The invention generally relates to an apparatus for adaptive signal processing and, in particular, an adaptive processor including beamforming and null-steering for an array antenna.
DESCRIPTION OF THE PRIOR ART Phase-coded spread spectrum communication ,signals may be acquired and synchronized in the presence of interference with the aid of an adaptive array antenna under the control of a well-known LMS (least mean square) algorithm performing power minimization. However, the signal to interference ratio at the adaptive array output port of a system using this type of processing, provides undesirable message quality which, at best, is o .<several decibels below the theoretical maximum obtainable when direction of arrival (beam steering) information is available.
4 In narrow band interference AM radios) communication systems, the spectral bandwidth of the interference source is significantly wider than the desired signal's bandwidth. Null-steering in such a case may be obtained by an LMS algorithm with spectral preconditioning of control signals of an adaptive processor to prevent null formation on the desired signal.
ny/ r M 2 SUMMARY OF THE INVENTION It is an object of this invention to provide an adaptive processor which performs simultaneously beamforming and null-steering.
It is another object of this invention to provide adaptive processing with a first adaptive control loop having off-epoch sample/hold filters and a second adaptive control loop having on-epoch sample/hold filters.
Therefore, the invention provides apparatus for cancelling undesired signals received with a desired spread spectrum signal, said apparatus comprising: first means for providing the desired and any undesired signal received with the desired signal; null-steering means, including a first temporal processing means associated with said first means, for Stemporally separating the desired and any undesired signals and cancelling at least a portion of any undesired signals; beamforming means, including a second temporal temporally separating the desired and any undesired signals and enhancing at least a portion of the desired signal; and second means for coordinating said null-steering means and said beamforming means; f i <7 I 3 wherein said first temporal processing means comprises a first adaptive control loop coupled to said first means, said first loop having a negative correcting I output for minimizing the undesired signal; ^said second temporal processing means comprises a second adaptive control loop coupled to said first means, said second loop having a positive correcting output for maximizing the desired signal; and said second means comprises means for summing the negative correcting output and the positive correcting output, and a mixer for mixing the desired and any undesired signals with the sum to provide a mixed output; j^1 further wherein said first adaptive control loop f comprises a first off-epoch sample-and-hold filter circuit coupled to the first means and providing an off-epoch unmixed output, a second off-epoch same-and-hold filter ^circuit coupled to the mixed output and providing an off-epoch mixed ouptut, and a correlator for correlating the off-epoch unmixed output with the off-epoch mixed output to provide said negative correcting output; and finally wherein each of said epoch filter I circuits includes means for tracking a desired signal, said tracking means including an early-gate and a late-gate overlapping a time of occurrence of the desired signal, there being an off-epoch gate and an on-epoch gate driven by said tracking means, for extracting samples of the desired signal and any interfering signal.
i V r 4 -4- BRIEF DESCRIPTION OF THE DRAWINGS In order that the invention may be more clearly understood, examples of preferred embodiments will now be described with reference to the accompanying drawings, in which: Figure 1 is a block diagram of an array antenna with adaptive processor according to an embodiment.
Figure 2 is a block diagram of a wideband spread spectrum temporal processor for one of a set of signal channels of Figure 1.
Figure 3 is a block diagram of an epoch processor of Figure 2.
Figure 4 is an array antenna pattern in the horizontal plane illustrating null-steering simulation.
Figure 5 is an array antenna pattern in the horizontal plane illustrating beamforming/null-steering simulation.
DETAILED DESCRIPTION OF THE INVENTION Figures 1-3 are single line block diagrams used generally to represent a vector system with multiple i signals. As used herein, references to a "line" are intended to generally mean multiple paths transmitting more than one signal. Similarly, references to "mixers" generally means multiplication with vectorial weights for combining multiple signals.
Figure 1 illustrates in block diagram form the general features of an embodiment of the invention.
Practice of the invention is demonstrated with reference to an array antenna 300 having four antenna elements 301, 302, 303, and 304 positioned for receiving an electromagnetic signal. It should be understood that, while the invention will be described with reference to reception of electromagnetic signals, the theory of the invention is applicable equally to the reception of sonic signals in which case the elements of the antenna would be transducers for converting sonic energy to electric energy. The four elements 301-304 of the antenna 300 are presented by way of example, it being understood that many more elements may be employed in practice. Also, in the general case, it is to be understood that the elements 301-304 may be positioned in a straight line or on a curved surface in accordance with the circumstances under which the antenna 300 is to be deployed. The situation in which the elements of the antenna 300 are to be positioned along a curved surface Is found in the locating of antenna elements on an aircraft in which case the elements may be positioned on the curved surface of a fuselage or wing of the aircraft.
Adaptive processing of input signals received at the elements 301-304 is accomplished by adaptive signal processors 305, 306, 307, and 308, respectively, coupled
LA,
0
XIA\
6 to the elements 301-304. Output signals of the processors 305-308 are applied to input terminals of a summer 309 which sums together the output signals of the processors 305-308 to output on line 310 a combined signal of the contributions of all of the elements 301-304 of the antenna 300. The output signal in line 310 is also fed back to each of the processors 305-308 to be used as a reference signal in the generation of weighting factors which are applied by the processors 305-308 in an adaptive fashion to the input signals of the respective elements 301-304 in accordance with the invention as will be described hereinafter.
It is noted that each of the processors 305-308 in combination with its respective antenna element 301-304 constitutes a separate signal processing channel, each channel sharing the summer 309 in common to provide the common reference signal on line 310. Each of these channels operates in the same fashion and comprises the same circuitry. Accordingly, in the ensuing description of the invention, the description will be directed to the 3 circuitry of one of the channels, namely the circuitry within the processor 305, it being understood that this description applies equally well to the other processors 306-308. The overall configuration of a set of processors sharing a common summer for weighting antenna signals is well known and need net be described further for an understanding of the embodiment. The embodiment resides with the circuitry of a single processor, such as the processor 305, as will now be described.
As shown in Figure 1, a desired signal with undesired signals interference) is provided by line to mixer 11. The desired signal with interference is also provided via line 12 to beamforming circuit 200 and via line 13 to null-steering circuit 100. The output of null-steering circuit 100 is provided via line 14 to coordinator 15 and added to the output of beamforming circuit 200 provided via line 16. The coordinated sum Is provided via line 9 to mixer 11, and further combined with the corresponding signals of the other channels by the summer 309, so that mixed output lines 310 and 17 carry the desired signal with interference mixed with the output of coordinator 15. This mixed signal is provided via line 18 to beamforming circuit 200 and via line 19 to null-steering circuit 100. Effectively, the null-steering circuit 100 functions as a first vector loop 1 to cancel at least a portion of the interfering signals.
Conversely, the beamforming circuit 200 functions as a second vector loop 2 to enhance at least a portion of the desired signal so that the mixed signal provided by line 17 has an enhanced S/I ratio and hence message quality.
The null-steering circuit and beamforming circuit may accomplish their functions by temporal -8 processing or by spectral processing. In the processing of phase-coded wideband spread spectrum communication signals, temporal processing may be employed as illustrated in a detailed diagram of the processor 305 in Figure 2.
As shown in Figure 2, the desired and interfering signals may be provided via line 10 to an automatic gain control circuit (AGC) 20 for stabilizing the signal amplitude. The output of AGC 20 is applied via line 21 to matched filter 22 and coded with the particular code of the desired signal. The output of matched filter 22 is provided via line 23 to first wideband vector weight control loop 1WB for null-steering and second wideband vector weight control loop 2WB for beamforming. In the first vector loop 1WB, the reference signal provided by line 24 and feedback signal provided by line 25 are processed by off-epoch sample/hold filter circuit 101 and off-epoch sample/hold filter circuit 103, respectively.
The processed signals are provided to correlator 102 for weighting the signal of antenna element 301 with the output of correlator 102 provided by line 106 to adder 28.
This effectively removes the desired signal from the control signal of a modified LMS algorithm effected in loop 1WB by correlator 102 with the minus sign in the vector loop 1WB shown at adder 28 representing r 9 implementation of a minimization process.
In the second vector loop 2WB, the reference signal provided by line 26 and the feedback signal provided by line 27 are processed by on-epoch sample/hold filter circuit 201 and on-epoch sample/hold filter circuit 203, respectively. The processed signals are provided to correlator 202 for weighting with the output of the correlator 102 provided by line 206 to adder 28. The second loop 2WB enhances the desired signal to modified LMS algorithm effected by correlator 202 with a net positive signal shown at adder 28 representing implementation of a maximization process.
Correlator 102 of vector loop 1WB comprises mixer 104 for mixing the output of the off-epoch circuits 101 and 103 and integrator 105 for integrating the mixed outputs. Correlator 202 of vector loop 2WB comprises mixer 204 for mixing the outputs of on-epoch circuits 201 and 203 and integrator 205 for integrating the mixed outputs. The output (line 106) of correlator 102 of loop 1WB is added to the output (line 206) of correlator 202 of loop 2WB by adder 28 and the sum is mixed by mixer 29 with the input signal provided by line 23 resulting in a mixed output signal provided by line 17.
The epoch processing circuits 101 and 201 are fabricated conveniently as a single unit 311 and, 11 \r jsimilarly, the epoch processing circuits 103 and 203 are fabricated conveniently as a single unit 312. Both of the units 311 and 312 have the same configuration and, accordingly, only the unit 311 need be described in H 5 detail, it being understood that the description thereof applies also to the unit 312. A unit 311 is found in each of the processors 305-308 of Figure 1. Also, a unit 312 may be placed in each of the processors 305-308 or, Salternatively, only one unit 312 need be provided for the H 10 entire antenna 300, with the output signals of the single unit 312 being employed by all of the processors 305-308.
With reference to Figure 3, there is shown a block diagram of epoch processing circuits contained within the unit 311, the description in Figure 3 applying tj 15 also to the epoch processing unit 312. Output signals are applied to the mixers 104 and 204 as shown in Figure 2.
The input signal to the epoch processing circuits are obtained from line 23 in the case of the unit 311, and from the line 17 in the case of the unit 312.
The unit 311 comprises an envelope detector 313, a threshold unit 314, a clock 315, a counter 316, and two signal generators 317 and 318 for producing an early-gate signal and a late-gate signal respectively. Input signals from line 23 are detected by the detector 313 which outputs the amplitude of the signal envelope to the threshold unit 314. The counter 316 counts clock pulses C- )~Y~-~r~M3FIMIU.*P^p~.~ 11 applied thereto by the clock 315. The threshold unit 314 outputs a command signal to the counter 316 during the interval of time when a detector 313 outputs a signal amplitude above the threshold of the unit 314. Thereby, the counter 316 is activated and deactivated to count the duration of a pulse of the input signal. The counter 316 strobes the generators 317 and 318. In the case of a repetitive input signal, as is the usual case in radar communication, the strobing of the generator 317 activates the generator 317 to output an early-gate signal, indicated graphically at 319, which extends in time from a point prior to the input signal pulse to the end of the input signal pulse. Similarly, the strobing of the generator 318 activates the generator 318 to output a large-gate signal, indicated graphically at 320, extending in time from a point at the beginning of the input pulse signal to a point after the conclusion of the input pulse signal. The two signals 319 and 320 overlap during the interval of time of the next anticipated occurrence of the input pulse signal.
The units 311 further comprises two gates 321 and 322, two low-pass filters 323 and 324, and a 12substractor 325. Both of the gates 321 and 322 have input terminals connected to the detector 313 for receiving signals outputted by the detector 313. The gates 321 is activated by the early-gate signal 319 of the generator 317 to pass detector signals to the filter 323 during the early-gate. The gate 22 is activated by the late-gate signal 320 of the generator 318 to pass detector signals :i to the filter 324 during the late-gate. The filters 323 and 324 average the signals applied repetitively by the gates 321 and 322. The average values outputted by the filters 323 and 324 are subtracted by the subtractor 325 to produce an error signal which indicates any error in the empl .acement of the gate signals 319 and 320 about an input signal pulse. The error signal is applied to the clock 315 to advance or retard the occurrence of clock pulses as commanded by the error signal, thereby to align the overlapping region of the gate signals 319 and 320 with the input signal pulse. Stylized representations of the signals outputted by the 'rly-gate 321 and the late-gate 322 are indicated at 326 and 327.
The unit 311 also comprises two gates 328 and 329, a delay unit 330 and a sunmer 331. The summer 331 provides an AND function between the early-gate signal 319 and the late-gate signal 320 to output a signal c2i line 332 having a value of logic-i during the overlap region of the two signals 319 and 320, and a value of lcgic-O otherwise, the overlap region between the two signals 319 13 and 320 is indicated graphically at 333. The logic-1 signal outputted by the summer 331 is indicated at 334.
The signal 334 indicates the expected time of arrival of the next input signal pulse on line 23, and Is applied to a terminal of the gate 329 to activate the gate 329 to conduct a signal from line 23 to the mixer 204.
This is termed the on-epoch part of the transmission of signals received by the antenna element 301. The signal 334 is also coupled via the delay 330 to a terminal of the gate 328 to activate the gate to couple signals from the line 23 to the mixer 104. The delay imparted by the delay unit 330 is sufficient to offset the activation interval of the gate 328 to a time after termination of the on-epoch of the gate 329. Accordingly, the interval of activation of the gate 328 is termed an off-epoch portion of the signal received at the antenna element 301.
In operation, the epoch processing circuitry of the unit 311 provides for tracking of the substantially periodic occurrences of pulses of the input signal outputted by the match filter online 23. The tracking of the input signal pulse is employed to operate the on-epoch gate 329 and the off-epoch gate 328 to provide samples of the signal energy during the times of receipts of the desired signal, and during the times wherein an interfering signal may be received. The off-epoch interval provides jamming data utilized by the loop IWB
S
C 0l' 3
I-
S14 (Figure 2) for directing a null in the direction of an interfering signal. The on-epoch interval provides energy of the desired signal which is employed by the loop 2WB (Figure 2) for maximizing the gain of the antenna 300 in the direction of a source of the desired signal. It is also noted that in the operation of the processor 305, that the integration operation of the correlators 102 and 202 converts the pulsed signal outputted by the epoch gates 328 and 329 to continuous signals applied to the adder 28 for formation of a continuously present weighting factor applied to the mixer 29. Thereby, the epoch processing circuits in conjunction with the correlators provide the adaptive control, loops with the characteristic of a sample-hold filter circuit with the temporal filtering being accomplished by the later and early-gate tracking operation.
Figures 4 and 5 illustrate the benefits of simultaneous null-steering and beamforming for a five-element random spaced array of antennas with an extent of 1 x 6 wavelengths in the azimuth plane and 2 wavelengths in elevation in a scenario consisting of three equal strength jammers (Jl, J2, J3) which are lOdB above o' the desired signal at each antenna: (0 1 ij Elevation Azimuth Sammer 1 (J1) 0° 0.40 Jammer 2 (J2) 00 22.30 Jammer 3 (33) 00 93.
80 S User 0° 62.20 Figure 4 is the adapted antenna pattern attained from a null-steering only control on the full signal band of frequencies for a loop bias condition which results in a single element "on" quiescent weight vector. In the adapted state, all the jammers are nulled by about and the desired signal(s) falls on the sides of a null which leads to a net improvement in S/J (signal to jammer) ratio of about 22dB. Figure 5 is the adapted pattern for the same scenario when the adaptive processor is configured employing both null-steering and beamforming.
In this adapted state, the null in the vicinity of the desir'ed signal(s) is filled in leading to an additional 6dB improvement in S/J ratio.

Claims (1)

16- THE CLAIMS DEFINING THE INVENTION ARE AS FOLLOWS: 1. Apparatus for cancelling undesired signals received with a desired spread spectrum signal, said apparatus comprising: first means for providing the desired and any undesired signal received with the desired signal; null-steering means, including a first temporal processing means associated with said first means, for temporally separating the desired and any undesired signals and cancelling at least a portion of any undesired A signals; beamforming means, including a second temporal processing means associated with said first means, for temporally separating the desired and any undesired signals and enhancing at least a portion of the desired signal; and second means for coordinating said null-steering means and said beamforming means; wherein said first temporal processing means comprises a first adaptive control loop coupled to said first means, said first loop having a negative correcting output for minimizing the undesired signal; said second temporal processing means comprises a second adaptive control loop coupled to said first means, said second loop having a positive correcting output for maximizing the desired signal; and 17 said second means comprises means for summing the negative correcting output and the positive correcting output, and a mixer for mixing the desired any undesired signals with the sum to provide a mixed output; further wherein said first adaptive control loop comprises a first off-epoch sample-and-hold filter circuit coupled to the first means and providing an off-epoch unmixed output, a second off-epoch sample-and-hold filter circuit to the mixed output and providing and off-epoch mixed output, and a correlator for correlating the off-epoch unmixed output with the off-epoch mixed output to provide said negative correcting output; and finally wherein each of said epoch filter includes means for tracking a desired signal, said tracking means including an early-gate and a late-gate overlapping a time of occurrence of the desired signal, there being an off-epoch gate and an on-epoch gate driven by said tracking means, for extracting samples of the I *desired signal and any interfering signal. 2. Apparatus as claimed in claim 1, wherein said second adaptive control loop comprises a first on-epoch sample-and-hold filter circuit coupled to the first means and providing an on-epoch unmixed output, a second on-epoch sample-and-hold filter circuit coupled to the mixed output and providing an on-epoch mixed output, and a correlator for correlating the on-epoch unmixed output with the on-epoch mixed output to provide said positive 18 correcting output; and wherein each of said on-epoch filter circuits includes means for tracking a desired signal, said tracking means including an early-gate and a late-gate overlapping a time of occurrence of the desired signal, there being an off-epoch gate and an on-epoch gate driven by said tracking means, for extracting samples of the desired signal and any interfering signal. 3. Apparatus as claimed in either of claims 1 or 2 and substantially as herein described with reference to any one of the examples shown in the accompanying drawings. DATED THIS 28th DAY OF June 1990 HAZELTINE CORPORATION By Its Patent Attorneys GRIFFITH HACK CO. Fellows Institute of Patent Attorneys of Australia i l I
AU14750/88A 1988-04-08 1988-04-19 Beamforming/null-steering adaptive array Ceased AU602974B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CA000563730A CA1325260C (en) 1982-05-28 1988-04-08 Beamforming/null-steering adaptive array
EP88303340A EP0337025B1 (en) 1988-04-08 1988-04-13 Beamforming/null-steering adaptive array

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AU1475088A AU1475088A (en) 1989-12-21
AU602974B2 true AU602974B2 (en) 1990-11-01

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4415282A1 (en) * 1994-04-30 1995-11-02 Sel Alcatel Ag Multipath reception radio receiver

Citations (3)

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Publication number Priority date Publication date Assignee Title
AU461398B2 (en) * 1971-05-13 1975-05-22 Nv pett. tps" GLOEILAMPENFABRIEKEN Filter for use ina carrier-wave measuring system
AU538974B2 (en) * 1980-07-10 1984-09-06 Newmont Mining Corp. Coherent noise cancellation
AU562044B2 (en) * 1984-04-20 1987-05-28 Matsushita Electric Industrial Co., Ltd. Audio noise reduction

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Publication number Priority date Publication date Assignee Title
US4079381A (en) * 1976-11-22 1978-03-14 Motorola, Inc. Null steering apparatus for a multiple antenna array on an AM receiver
US4156877A (en) * 1978-01-16 1979-05-29 Motorola, Inc. In null steering apparatus a reference to spread spectrum signals
US4225870A (en) * 1978-05-10 1980-09-30 The United States Of America As Represented By The Secretary Of The Army Null steering antenna
US4173759A (en) * 1978-11-06 1979-11-06 Cubic Corporation Adaptive antenna array and method of operating same
US4651155A (en) * 1982-05-28 1987-03-17 Hazeltine Corporation Beamforming/null-steering adaptive array
US4516126A (en) * 1982-09-30 1985-05-07 Hazeltine Corporation Adaptive array having an auxiliary channel notched pattern in the steered beam direction

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU461398B2 (en) * 1971-05-13 1975-05-22 Nv pett. tps" GLOEILAMPENFABRIEKEN Filter for use ina carrier-wave measuring system
AU538974B2 (en) * 1980-07-10 1984-09-06 Newmont Mining Corp. Coherent noise cancellation
AU562044B2 (en) * 1984-04-20 1987-05-28 Matsushita Electric Industrial Co., Ltd. Audio noise reduction

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AU1475088A (en) 1989-12-21
DE3885089T2 (en) 1994-05-19
EP0337025A1 (en) 1989-10-18
DE3885089D1 (en) 1993-11-25
JPH01293002A (en) 1989-11-27
EP0337025B1 (en) 1993-10-20

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