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Radar Detection
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Radar Lecture @ Prof Y Kwag Korea Aerospace Univ. RSP Lab
Chapter 4
Radar Detection
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
4.1 Detection in the Presence of Noise
RSP Lab
Detection in the Presence of Noise
Fig 4.1. Simplified block diagram of an envelope detector and threshold receiver
2variancewithnoise,Gaussianwhitemeanzeroadditive:)(
signalechoradar:)(where
)()(signalinput
tn
ts
tnts
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
RADAR DETECTION
RSP Lab
- Band pass IF filter output signal is
)/tan()(
)1.4()(ofenvelope)(where
)(sin)()(,)(cos)()(
))(cos()(sin)(cos)()( 000
IQ
QI
QI
vvaphaset
tvtr
ttrtvttrtv
tttrttvttvtv
alarmMissVtnts
alarmFalseVtn
DetectionVtnts
T
T
T
)()(
)(
)()(
Radar designers seek to maximize the probability of detection for a given
probability of false alarm
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
RADAR DETECTION
RSP Lab
- If filter output is composed of
noise alone
)2.4()()(,)()( tntvtntv QQII
noise plus target return signal (sine wave of amplitude A)
)3.4()(sin)()()(
)(cos)()(cos)()()(
ttrtntv
AttnttrtnAtv
III
Where the noise quadrature components and are uncorrelated zero mean
Low pass Gaussian noise with equal variance, .
)(tnI )(tnQ
2
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Joint probability density function
RSP Lab
- The joint probability density function (pdf) of the two random variables is QI nn ,
)4.4(2
)sin()cos(exp
2
1
2exp
2
1),(
2
22
22
22
2
rArnnnnf
QI
QI
- The pdf of the random variable and , represent the modulus and phase
of . The joint pdf for the two random variables is
)(tr )(t
)(tv )(,)( ttr
)8.4(cos
exp2
exp2
),(
)7.4()(casethisin
)6.4(cossin
sincosjacobian:where
)5.4(),(),(
22
22
2
rAArrrf
trJ
r
r
n
r
n
n
r
n
J
Jnnfrf
II
QI
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Rice probability density function
RSP Lab
- The pdf for r alone is obtained by integrating over ),( rf
2
0
22
22
2
2
0
cosexp
2
1
2exp
),()(
drAArr
drfrf
Where the integral inside Eq.(4.9) is known as the modified Bessel function
of zero order.
)10.4(2
1)(
2
0
cos
0
deI
Thus,
2
22
202 2exp)(
ArrAI
rrf
Rice probability density function.
)11.4(
)9.4(
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Rayleigh & Gaussian pdf
RSP Lab
)11.4(2
exp)(2
22
202
ArrAI
rrf
- Rice pdf
pdfRayleighpdfRiceA thebecames),alonenoise(0If- 2
.varianceandmeanofathebecames
,largeveryisIf-
2
2
ApdfGaussianpdfRice
A
)12.4(2
exp)(2
2
2
rrrf
)13.4(2
)(exp
2
1)(
2
2
2
Arrf
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Rayleigh & Gaussian pdf
RSP Lab
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Rayleigh & Gaussian pdf
RSP Lab
- The density function for the random variable is
* Note that for the case of noise alone (A=0), Eq.(4.15) collapses to
a uniform pdf over the interval {0, 2}.
drrff
r
0
),()(
cos
2
)sin(exp
2
cos
2exp
2
1)(
2
2
22
2 AF
AAAf
x
dexFwhere
22
2
1)(
)14.4(
)15.4(
)16.4(
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Rayleigh & Gaussian pdf
RSP Lab
- One excellent approximation for the function F(x) is
02
1
51.5339.0661.0
11)( 2
2
2
xe
xxxF x
xofvaluesnegativeforand
)(1)( xFxF
)17.4(
)18.4(
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
4.2. Probability of False Alarm
RSP Lab
Probability of False Alarm
- Probability of false alarm is define as the probability that a sample
of the signal will exceed the threshold voltage when noise alone.
faP
R )(tr TV
levelthresholdtheinchangessmall
tosensitiveveryisPfa
2
2
2
2
2 2exp
2exp
T
V
fa
Vdr
rrP
T
)19.4( a
fa
TP
V1
ln2 2 )19.4( b
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
4.2. Probability of False Alarm
RSP Lab
Fig 4.3. Normalized detection threshold versus probability of false alarm
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
False Alarm Time
RSP Lab
- The false alarm time is faT
- Since the radar operating bandwidth is the inverse of B intt
Maximizing increasing decreased faT TV max)( dR
fa
intfa
P
tT )20.4(
voltaged threshol thepass willdetector envelope theofouput the
thattimeaverageortimenintegratioradarwhere intt
)21.4(
2
2
2exp
1
T
fa
V
BT
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
MATLAB function que_func.m
Compute -function [PD] = marcumsq(a, b)
-This function uses Parls method to compute PD
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
4.3. Probability of Detection
RSP Lab
Probability of Detection - Probability of detection is the probability that a sample of will exceed
the threshold voltage in the case of noise plus signal
DP )(trR
)22.4(2
exp2
22
202dr
ArrAI
rP
TV
D
- Assume that the radar signal is a sine waveform with amplitude A, then its power
is . By using (single-pulse SNR) and . 22A 22 2ASNR )1ln()2(
22
faT PV
)24.4()(,
)23.4(1
ln2,2
exp
2/)(
0
2
2
)/1ln(2
2
22
202
22
2
deIQ
P
AQdr
ArrAI
rP
faP
D
fa
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Probability of Detection
RSP Lab
- Many approximations for computing Eq.(4.23). Very accurate approximation
presented by North is given by
- Q is called Marcums Q-function. When is small and is large so that the
Threshold is also large, Eq.(4.24) can be approximated by
faP DP
fa
DP
AFP
1ln2
)25.4(
5.0ln5.0 SNRPerfcP faD )26.4(
isfunctionerrorarycomplementthewhere
z
v dvezerfc0
221)(
)27.4(
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Table 4.1 Single Pulse SNR(dB)
RSP Lab
dBSNRPandP faD 12.16pulsesinglemin.1099.010
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Example 4.1
RSP Lab
dBSNR
FigandTablefromand
BTP
nB
solution:
le pulse.f a singhe SNR o , and t alarm P of falseobability , the prtime t
ration dar integd the ra1GHz. FinBandwidth 0.9 and bection Py of detprobabilit
e 16.67minutrm T false ala: time ofification wing specthe follodar has pulsed raA
fa
fa
faint
D
fa
75.15)(
4.4.1.4
106067.1610
11
sec110
11t
1
12
9
9int
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Probability of Detection vs single pulse SNR
RSP Lab
Compute - This program us used to produce Fig. 4.3 with marcumsq.
10-2
10-4
10-6
10-8 10-10 10-12
15.75dB
Assume
Tfa=16.67minutes, PD=0.9,
(SNR)1 ?
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
4.4. Pulse Integration
Radar pulse integration
: adding radar echoes from many pulses
(1) Coherent (Pre-detection) integration
perform on the quadrature components prior to the envelop detection
(2) Non-coherent (Post-detection) integration
perform after the envelop detector
RSP Lab
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Coherent Integration
RSP Lab
Coherent Integration Perfect integrator using Integrating np pulses improve the SNR
The case for non-coherent integration integration loss
- mth pulse
)()( tntsy mm (4.34)
)(ts
)(tnm
: radar return of interest
: white uncorrelated additive noise signal
- Coherent integration of np
(4.35)
ppp n
m
m
p
n
m
m
p
n
m
m
p
tnn
tstntsn
yn
tz111
)(1
)()]()([11
)(
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Coherent Integration
RSP Lab
(4.36)
(4.37)
- Total noise power in z(t) = variance
2
1,
2
21,
*
2
2 11)]()([1
ny
p
n
lm
mlny
p
n
lm
lm
p
nznn
tntnEn
pp
*
11
2 )(1
)(1 pp
n
l
l
p
n
m
m
p
nz tnn
tnn
E
2
ny : single pulse noise power
: 0 (ml) , unity (m=l) ml
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Coherent Integration
- The desired signal power after coherent integration : not change
noise power is reduced by 1/np
RSP Lab
- SNR after coherent integration : Improve np
- Single pulse SNR : (SNR)1 ,
- Integrated (np) pulse SNR : (SNR)np
- SNR after coherent integration : improve np
1)(1
)( SNRn
SNRp
np (4.38)
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Non-Coherence Integration
Non-Coherence Integration
RSP Lab
: Non-Coherence Integration : implemented after the envelope detector
Fig 4.5. Simplified block diagram of a square law detector and non-
coherent integration
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Non-Coherence Integration
RSP Lab
- Square law detector used as an approximation to the optimum receiver
- Define a dimensionless variable (y)
/nn ry
SNRA
Rp 22
2
(4.39)
(4.40)
- The pdf for the new variable
2
)(exp)()()(
2
0
pn
pnn
n
nnn
RyRyIy
dy
drrfyf
(4.41)
2
2
1nn yx
(4.42)
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Non-Coherence Integration
RSP Lab
- The pdf for the variable at the output of the square law detector
pnpnn
nnn RxI
Rx
dx
dyyfxf 2
2exp)()( 0
(4.43)
- Non-coherent integration of np pulses
pn
n
nxz1
(4.44)
- xn are independent, the pdf for variable z
(4.45) )()()()( 21 pnxfxfxfzf
: the modified Bessel function of order
ppnppn
pp
zRnIRnzRn
zzf
p
p
22
1exp
2)( 1
2/)1(
(4.46)
1p
n1pnI
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Non-Coherence Integration
RSP Lab
1)(
)()( 1
pnp
pSNRn
SNRnE
- Non-Coherent integration efficiency
(4.47)
- Integration improvement factor for a specific Pfa
ppp
n
p nnEnSNR
SNRnI
p
)()(
)()( 1
(4.48)
- An empirically derived expressed for improvement factor
(accurate within 0.8dB)
(4.49)
2)log(018310.0)log(140.01
)log(6.46
)/1log(1)235.01(79.6)(
pp
p
fa
DdBp
nn
nP
PnI
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Non-Coherence Integration
RSP Lab
Fig 4.6. Improvement factor VS number of pulses (non-coherent integration).
These plots were generated using the empirical approximation in Eq.(4.49).
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
4.5. Detection of Fluctuating Targets
RSP Lab
Detection Probability Density Function - probability density function for fluctuating targets
0exp1
)(
A
A
A
AAf
avav
02
exp4
)(2
A
A
A
A
AAf
avav
Swerling I & II
Swerling III & IV
(4.50)
(4.51)
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Detection of Fluctuating Targets
- Performing the analysis for the general case
RSP Lab
2
2
12
22/)1(
222
2
1exp
)/(
2)/(
AznI
Anz
An
zAzf pnp
n
pp
p
(4.52)
- To obtain f(z) use the relations
)()/(),( AfAzfAzf
- Finally,
(4.53)
(4.54)
dAAzfzf ),()(
(4.55) dAAfAzfzf )()/()(
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Detection of Fluctuating Targets
Threshold Selection
RSP Lab
- DiFranco and Rubin general form relating the threshold and Pfa for any
number of pulsed and non-coherent integration
- Incomplete Gamma function
1,1 p
p
Tlfa n
n
VP
dn
en
n
V pT pnV
p
n
p
p
Tl
/
0
11
)!11(1,
1
2
1
)!1(
)2)(1(11
)!1(11,
p
Tp
n
T
p
T
pp
T
p
p
Vn
Tp
p
Tl
V
n
V
nn
V
n
n
eVn
n
V
- Approximated,
(4.56)
(4.57)
(4.58)
RSP Lab Hankuk Aviation Univ.
Threshold vs TV pn
10 100
19.11
Nfa = Marcums false alarm number nfa : pfa
30.05
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
4.6. Probability of Detection Calculation
- Single pulse SNR is unity (0 dB) range R0 (reference range)
RSP Lab
14
4
00
3
22
0
BFLRkT
GPSNR tR
4003
22
4 BFLRkT
GPSNR t
4
0
0
R
R
SNR
SNR
R
- Single pulse SNR at any range R
- Dividing Eq.(4.66) by Eq.(4.65)
(4.65)
(4.66)
(4.67)
R
RSNR dB
0log40
- SNR at any other range R
(4.68)
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Detection of Swerling I targets
Detection of Swerling I Targets
- detection probability for Swerling I type targets (derived by Swerling)
1
1 pSNRV
D ; nePT
11,1
1
111,1
1
1
p
SNRnV
p
p
TI
n
p
pTID ; nen
SNRn
V
SNRnnVP pT
p
(4.76)
(4.77)
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
2 4 6 8 10 12 14 16 18 20 220
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1
SNR - dB
Pro
babili
ty o
f dete
ction
Swerling V
Swerling I
Probability of detection versus SNR,
single pulse. Pfa= 910
Swerling I and V type fluctuating np=1
Matlab Function pd_swerling1.m
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
-10 -5 0 5 10 15 20 25 300
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1
SNR - dB
Pro
babili
ty o
f dete
ction
np = 1
np = 10
np = 50
np = 100
Probability of detection versus SNR,
Swerling I. Pfa= 610
Matlab Function pd_swerling1.m
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
-10 -5 0 5 10 15 20 25 300
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1
SNR - dB
Pro
babili
ty o
f dete
ction
np = 1
np = 10
np = 50
np = 100
Probability of detection versus SNR,
Swerling I. Pfa= 1210
Matlab Function pd_swerling1.m
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Detection of Swerling II targets
Detection of Swerling II Targets - detection probability for Swerling II type targets
50,
11
pp
TID ; nn
SNR
VP
- When np>50, Eq.(4.70) is used to compute detection probability
pnC
3
13
SNRnp 1
PnC
4
14
2/2
36 CC
(4.78)
(4.79)
(4.80)
(4.81)
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
-10 -5 0 5 10 15 20 25 300
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1
SNR - dB
Pro
babili
ty o
f dete
ction
np = 1
np = 10
np = 50
np = 100
Matlab Function pd_swerling2.m
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Detection of Swerling III targets
Detection of Swerling III Targets
- detection probability for Swerling III type targets (derived by Marcum)
- when np=1, 2
op
pp
T
n
pp
TD Kn
SNRnSNRn
V
SNRnSNRn
VP
p
22
2/11
21
2/1exp
2
1,/21
1,1!22/1
0
1
p
p
TIpTI
pp
Vn
TD n
SNRn
VKnV
nSNRn
eVP
Tp
- for np>2
(4.82)
(4.83)
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Matlab Function pd_swerling3.m
RSP Lab
-10 -5 0 5 10 15 20 25 300
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1
SNR - dB
Pro
babili
ty o
f dete
ction
np = 1
np = 10
np = 50
np = 100
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Detection of Swerling IV targets
Detection of Swerling IV Targets
- detection probability for Swerling IV type targets (derived by Marcum)
- for np
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Matlab Function pd_swerling4.m
-10 -5 0 5 10 15 20 25 300
0.2
0.4
0.6
0.8
1
SNR - dB
Pro
babili
ty o
f dete
ction
np = 1
np = 10
np = 50
np = 100
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
4.7. Cumulative Probability of Detection
RSP Lab
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
4.7. Cumulative Probability of Detection
- The cumulative probability of detection refers to detecting the target at least
once (range R)
- The target gets closer to the radar, probability of detection increases
- The probability of detection during the n th frame is PDn ,
Then, cumulative probability of detecting during n th frame is
RSP Lab
)1(11
n
i
DC inPP (4.95)
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
Prob 4.3. A radar detects a closing at R, PD= 0.5 , Pfa=10-7. Compute and
sketch the single look probability of detection as a function of range
(interval 2~20 Km) If successive frame is 1Km, cumulative
probability of detection at 8Km ?
RSP Lab
Example 4.3
RR
SNRSNR R log405210
log40)()( 10
Sol) From table 4.1 the SNR corresponding to PD= 0.5 , Pfa=10-7 is 12dB.
From eq. (4.68) , the SNR at any range R as
-The cumulative probability of detection at 8Km is
9998.0)1)(01.01)(07.01)(25.01)(5.01)(9.01)(999.01(1 39
CP
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ. RSP Lab
Example 4.3
< PD versus normalized range>
frame 1 2 3 4 5 6 7 8 9
Range in Km 16 15 14 13 12 11 10 9 8
< range listing for frames 1 through 9 (frame 9 corresponds to R = 8Km) >
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
4.8 Solving the Radar Equation
RSP Lab
4
1
0
3
2
)()4(
SNRFLkT
GGTfPR
e
rtirt
gain antennareceivingG
gain antennangtransmittiG
tervalindwellT
PRFf
widthpulse
power dtransmittepeakP
r
t
i
r
t
(4.96)
detectionfor requiredSNRminimum(SNR)
figure noisereceiver F
emperaturereceiver tT
constant sBoltzmnn'k
loss systemtotalL
section crosstarget
wavelength
0
e
where,
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ. RSP Lab
4.8 Solving the Radar Equation
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
4.9 Constant False Alarm Rate (CFAR)
RSP Lab
fa
TP
V1
ln2 2
- Relationship between threshold value VT and Pfa
- The process of continuously changing the threshold to maintain a constant
=> Constant False Alarm Rate (CFAR)
Three different types of CFAR
Adaptive threshold CFAR ( assume that interference distribution is known)
Nonparametric CFAR ( unknown interference distribution )
Nonlinear receiver techniques ( normalize root mean square of interference )
(4.97)
powernoisewhere 2,
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ. RSP Lab
4.9.1 Cell-Averaging CFAR (single pulse)
< Conventional CA-CAFR >
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ.
- The echo return for each pulse is detected by a square law detector
- The Cell Under Test (CUT) is the central cell
- The neighbors of the CUT are excluded from average process due to
spillover
- The output of M reference cells is averaged
- The threshold value is obtained by averaged estimate all reference cell by K0
RSP Lab
4.9.1 Cell-Averaging CFAR (single pulse)
ZKY 01
- Cell-averaging CFAR assumes all reference cells contain zero mean
independent Gaussian noise of variance
- In this case, the gamma pdf is,
0;)2/(2
)(2/
)2/(1)2/( 2
zM
ezzf
MM
zM
(4.98)
(4.99)
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ. RSP Lab
4.9.1 Cell-Averaging CFAR (single pulse)
- The conditional probability of false alarm when y= VT can be written as 22/)( yTfa eyVP
- The unconditional probability of false alarm is
dyyfyVPP Tfafa
0
)()(
where, f(y) is the pdf of threshold,
- Except for the constant K0 is the same as (4.99). Therefore,
0;)()2(
)(2
0
)2/(12
0
yMK
eyyf
M
KyM
Mfa KP
)1(
1
0
- Substituting (4.102) and (4.100) into (4.101) yields
(4.101)
(4.100)
(4.102)
(4.103)
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ. RSP Lab
4.9.2 Cell-Averaging CFAR with Non-Coherent Integration
< Conventional CA-CFAR with non-coherent integration>
Radar Lecture @ Prof Y Kwag Korea Aerospace Univ. RSP Lab
4.9.2 Cell-Averaging CFAR with Non-Coherent Integration
- The output of each reference cell is the sum of nP squared envelopes
- Total number of summed reference samples is MnP
- The output Y1 is also the sum of nP squared envelopes
- Noise alone is present CUT, Y1 random variable (pdf with 2 nP degrees of
freedom)
- The probability of false alarm is equal to the probability Y1 /Z exceeds threshold
11 /Pr KZYobPfa
- Let conditional probability of false when y= VT be Pfa (VT = y),
unconditional false alarm probability is,
dyyfyVPP Tfafa
0
)()(
where, f(y) is the pdf of the threshold
(4.104)
(4.105)