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Radar Equation
 
2.1 Prediction of Range Performance
+ The maximum radar range ar is given by ae form of expression.
y
heh eae
Ree - ge)" ‘oe Ne om Sen (2.1.1)
7)" Prin Tats Gi dh e,
Where, aie he
P, is peak value of transmitted power
G, is power gain of transmitting antenna. Li%
@ is area of cross-section of target (m?)
Prin is minimum detectable signal by receiving antenna. (W)
* The radar equation shows that different parameters of radar system can be
controlled except target cross-section area (c). When long range is desired,
the transmitted power (P)) should be large, the transmitting gain must be
large, also the receiver should be sensitive to weak signals.
* However the above radar equation may not give predict actual performance
of radar. In practice, the radar performance degrades because of following
reasons.
The minimum detectable signal is determined by receiver noise.
Fluctuations and uncertainty in radar cross-section.
Losses in various parts of radar system.
Propagation effects due to earth’s surface and atmosphere.
Encepl fete totgct Aacsscchion
ae
cL RCS, all he OMe loccqres
Urls We . 2 1) Combes of KADAR
 
Fens
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2-2
Radar Systems
e and target cross-section, the
¢ of receiver noise an
ccs a decked probabilistically rather than single
ange is de i
SSE GRIEE rac range specication includes
i : e.
Sasi that radar will detect a target at a particular range.
4 Probability of making a false detection when no target is present.
i the range of radar is a function of
facts it can be concluded that the rang
ae i bability of false alarm (Pj). The
lity of detection (P,) and the probability
Prediction of radar range is not accurate as there is uncertainty in various
Parameters, Still radar range equation is an important tool for
') Assessing the performance of radar.
1) "Determining system tradeoffs for designing a new radar system.
iti) Generating technical requirements for new radar procurement,
22 Minimum Detectable Signal
The radar receiver's abil NB 4 Weak echo signal is decided by the
noise present in the frequency spectrum, The weakest signal that a radar can
detect is minim, is
lum dete le si i A
denoted by p stectable signal. The min mum detectable signal is
{ Deection ‘of radar gan ishit
carn OF Padar sign '8 based’ on sstablishing threshold ley,
= receiver. A target is said to be Present when the
ger than the threshold, If the receiver output is below
noise iN Teceiver, it is called as threshold detecti
a re town it Fig. 3.94, This output een 2
€ Versus tiy is i
a time, it ig fluctuating because rand. _:
‘el for the
Teceiver output is
 
 
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a, ube Picce tee signal plus noise. When a large echo signal
po erect it Is represented by ia patted
ly, the output level does y A. If the threshold level is sett
Not exceed threshold if noise only is present
and it should exceed threshold when Strong echo is present. Lab
a) Missed detection (failing to Tecognize a tar
+ The signal-to-noise ratio (SNR) j
of a radar instead minimum detectable signal.
2.3 Receiver Noise and SNR
+ The noise affects the maximum radar range as it determines the minimum
_ teceved power that radar can detect. Als, tie Tadar epee ee
by decreasing minimum detectable power which depends on the sensitivity
the receivers and hence on its noise figure. Noise figure F, is defined as
Rae. _Input signal to noise ratio ~~
Output signal to noise ratio
  
 
  
 
  
 
the definition of the noise figure, the noise power generated at the
Of receiver can be calculated. Thus the power required at the input of
ideal receiver having the same noise figure as the practical receiver
   
F = S)input
GIN) output
Fea te Poo
F
Fe
aie
ig . ual
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2-4
a
where,
Pg ~ Input signal power
Py = Output signal power
Pa, = Input noise power
Pao ~ Output noise power
G, - Power gain of receiver “eg
Pari - Noise power generated at the receiver input
re
therefore ai = (F=1)
 
 
 
Poi = Ty BF
 
where, KT) B = Noise input power of receiver
K = Boltzmann's constant
= 138x109 9/K
Ty = Ambient temperature = 290 K
B = Bandwidth of the receiver, Hz
* Im the above equation it is assumed that antenna temperature is equal to the
standard ambient temperature. The actual antenna temperature is important
when a very low-noise amplifier is used.
* Under threshold detection conditions, the minimum detectable signal is equal
to the equivalent noise power at the input of receiver.
. The ‘echoes from the target are repetitive, whereas noise impulses are
random. Thus an integration of echoes takes place at the receiver,
echo pulse can be obtained although their amplitude is no greater than that
of noise impulses. When the target is stationary, the signal pulses keep on
accumulating at the same spot so that the brightness at this spot of the
Screen is maintained, whereas the noise impulses are of pure random in
nature and are not additive.
+ If the target is moving and it moves significantly between successive scans, a
system called moving-target-indicator is used. Therefore minimum
signal Pian Should be atleast equal to.
Pyin = KT B(F-1)
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ee ee
The radar range equation is
 
Substituting Pain in radar range equation
(4x)? KT) BF-1)
 
 
 
  
 
 
+ The radar range can be predicted fairly accurately
E ly using above equation. Still
there are other factors which affect the radar range and for very accurate
calculations these factors have also to be considered. These factors include :
a) System losses
b) Receiver non-linearities
©) Antenna imperfections
d) Anomalous propagation
¢) Interference by nearby noise sources
) Operators error
Since Gre -the
2
And Ae= nA
ae (]
re xD? xD
G = 4xx Sey -005(2Y
 
Also Ty = 290° and K = 138x 10-9 J/°K
* The expression for maximum radar range is
PD's Va
toe [ar
where, P, - Peak transmitted power, watts
D - Diameter at antenna, metres
9 - Effective cross-sectional area of target, metre”
B - Bandwidth of receiver, Hz
af
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a.i
patente - er
A - Wavelength, m
F - Noise figu
 
ym> Example 2.3.1: Calculate the minimum receivable signal in a radar receiver operating in
standard ambient temperature, which has an IF bandwidth of 2 MHz and a noise figure of
12 4B.
Solution : B = 2 MHz = 2x 10° Hz
F = 12dBs
12
F = Antilog 55
F = 15.84
Minimum receivable signal is given by,
Pmin = K Ty BF - 1)
K = 138x109 J/*
T = 20%
Poe 10° 3 x 290 x 2 x 10° [15.84 - 1]
Prin = 118.85 x 10” watts «Ans.
i.
 
mp Example 2.3.2: A low power radar has a receiver whose noise figure is 5.3 aB. If the
antenna diameter is 1.5 m, the IF bandwidth is 500 kHz, the operating frequency is 8.1 GHz
and the radar set is supposed to be capable of detecting targets of 5 m° cross-sectional area at
a maximum distance of 15 km. What must be the peak transmitted power ?
Solution : F=53 dB
D=15m
B = 500 kHz = 500x 10° Hz
f = 81 GHz = 81x10? Hz
o = 5m
Rmax = 15 km
PR = to find
Since F = 53 dBs
 
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=
5.3
= Antilog 2
Antilog 3
F = 3.388
And
 
c
i
3x108
= oxi = 0.037
Ano a
Maximum range of radar and transmitted power are related by equation
note
eet
a [3 ~ |
 
where Ruy is in km
 
 
 
 
PD‘
BA(F-1)
 
BA(F-1) (15 ¢
Paes) (15
Dis (#8
p, = 300x108 x(0.037)?(3.388-1) (15
oy 154 x5 48
 
0.6158 watts Ans,
ay
ump Example 2.3.3: A radar system operates at 6 GHz 3 MW power output. If the antenna
diameter is 5 m and the receiver bandwidth is 1.5 MHz and has a 12 dB noise figure, what
is the maximum detection range for 1 m? target.
Solution : F = 6 GHz
P, = 3MW=3xx 10° watt
D = 5 metres
1.5 MHz = 15x 10° Hz
F = 12dB
o=1m
c
Eta
4 mai
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Hadar Enysation
Radar range equation is given by,
L [t Ge mu
iar Tus} 20 ee
Ri. AGio eaiieaille |
(49)? Prain ’
G? = REA? Pin
Pio
R449)? Prag JE
Gy = [RE Pain
Pio
1
3x10° x(0.24)? x1
Gy = 1643.76
"Also for paraboloid effective area is given by,
 
Se 1643.76 x (0.24)? .
b xx |
A, = 753
The effective area A, is related with physical area A by relation
Ae = nA
753 = 065% A
a A = 1159
4 a
‘Area of paraboloid A =
xD?
Fp us
ba D = 38tmere Ans.
 
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8
ee pia eon
; Radar Equation
f signal energ:
ton scienes, Hal beed energy during tectification process. The
Ot Post-detection integration is, given b
(9), ration is given by,
© © nN) (244)
same integrat )
« For Brated SNR, post-detection integration requires more pulses
een ore spsuming SNR per pulse is same in both cases. When
a edetecian ni integrated (small SNR per pulse), the difference
between predetection and post detection is significant
«The radar equation with n pulse integrated is given by,
: RGA |
GaKn aN,
 
Rina
 
(245)
where,
(i), is signal-to-noise ratio of each pulse.
25 Radar Cross-Section (RCS) of Targets
* The amount of power reflected by the target depends on many factors
including the size, shape, material (metal, plastic, wood or water) and edges
(sharp or rounded) of the target, as well as the frequency of the incident
radar signal and the angle between the radar system and the target.
* The radar cross-section 6 is the property of a scattering object which
represents the magnitude of the echo signal returned to the radar by the
target.
* The radar cross-section depends on the characteristic dimensions of the object
compared to the radar wavelength. When the wavelength is large compared
me to the object’s dimensions, scattering is said to be in Rayleigh region. The
radar cross-section in the Rayleigh region is proportional to the fourth power
of the frequency.
* When the wavelength is small compared to the object's dimensions is called
the optical region.
* In between the Rayleigh region and optical regions is the resonance regions,
where the radar wavelength is comparable to the objects dimensions
(approximately 1 to 10 wavelengths).
it
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b, = Pinoy i
"phe or For perfectly conducting sphere
where,
jn iS spherical Bessel function of the first kind.
Nh? is spherical Hankel function of second kind,
nis summation counter.
 
2
&
o
4
Bos
Mie or Resonance region
  
 
 
0.05 o4 02 05 1
Circumference
a=
2) ==>
Fig. 2.5.1
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Fig. 2.5.2
cross-section of cone sphere is a very low and is considéred to be of
7 missile. A large cross-section occurs when a radar views the cone
¢ ws ’
rage transmitter power is defined over the duration of total transmission
d. The transmitted waveform is a train of rectangular pulses of width t
pulse repetition period Tp.
fs pe repetion fequency
«tie at
Thy
od A
UP at i
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8
(x | = SNR required as if direction were based on only single
Pulse
f, = Pulse repetition frequency (Hz)
2.7 PRF and Range Ambiguities
«PRE is uy determined by maximum unambiguous range. The PRF
corresponding to maximum, unambiguous range is given by,
= 2Runambiguous
—aenbigwoe
 
where,
cis velocity of Propagation.
«Echo signals that are received later than pulse repetition period are known as
second time around echoes or multiple time around echoes. These echoes
may cause error and confusion. Also it can mask unambiguous target echoes
at shorter ranges. Pulse doppler radars have usually problem of range
ambiguities because of prf. The problem of multiple time around echoes
occurs when the range is greater than 2 Runambiguous: These echoes cannot be
determined from constant prf-———"6*
* Consider the targets located at three different positions A, B and C as shown
in Fig. 27.1.
Ais located within unambiguous range interval Rusanbiguose
Bis located at a distance > Ruranbiguow but less than 2 wanbiguou
Cis located at a distance > 2. Rusanbiguou but less than 3 Reranbiguour
* Fig. 27.1 (a) shows target B is a second time around echo and target C is
_ multiple time around echo. Fig. 27.1 (b) shows radar display when these
_ three pulse repetition intervals are superimposed. The ambiguous echoes B
and C looks very similar to unambiguous range echo of A. Out of these
three echoes only the range of A is correct but it is hard to determine that
‘other two are not the apparent ranges,
The ambiguous range echoes are recognized by changing the prf of the
-tadar. On changing the prf, the unambiguous echo ( 2.0 dB
(CFAR)
Automatic integrator 1.5 to 2.0 dB
 
1.0 to 2.0 dB
 
 
Upto 1 dB
  
   
   
  
   
 
2.8.4 Collapsing Loss
* When additional noise samples are integrated with signal + noise pulses, this
added noise causes degradation called collapsing loss.
The collapsing loss is given by L.
i(m+n)
Le
where, ‘
Licmen) is integration loss for m+n pulses.
Li(a) is integration loss for n pulses. —
'm is noise pulses.
nis signal - to - noise pulses.
 
Le¢mn)
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30 noise pulses. If integration lose
Toss due to noise pulses (10) is 1,7
solution : Given
leclor integrates 10 signal plus noise pulses along with
for signal + noise pulses (40) 18 3.5 dB and integration
4B. Calculate collapsing loss of the radar antenna.
Signal plus noise pulses (m) = 10
Noise pulses (n) = 30
Integration loss L. = 35 4B
(men) =
Integration loss Li.) = 1.7 4B
Collapsing loss is ee,
i(m+n)
Lion
 
Lomeny =
o
a
Lemen) =
Q
  
   
  
    
 
  
    
   
Effects
‘The propagation effects of radar wave has significant impact on losses. Major
of propagation on radar performance are under mentioned.
Reflections from earth's surface "i
Refraction
Propagation in atmospheric ducts
Attenuation in clear atmosphere.
Te propgation efits are mot computed under astm ls but under
2
 
  
Radar range equation is an important todl for
i) Assessing radar performance
ii) Designing radar system
iii) Generating technical requirements
a
@ scanned with OKEN ScannerF Sdection of proper threshold is necessary
) Missed detection
. ‘of pulses returned after hitting target is given by,
3. Number of pu!
eal
n= =
- . of summing all the radar echoes
pulses is the process
 
4. The integration of
oa of pied before second detector is known as predetection
5. The integra j
integration or coherent integration.
6 The integration of pulses after second detector is known as post detection or
coherent integration.
7. Integration efficiency for post detection integration
   
 
  
e,. « On
*) “ 2G),
8. Radar cross-section (RCS) is given by
2
is 2 LErl
° ae peat
  
9. RCS for sphere is given by, A
o= 2) Sirens (en ho)
P lnat
10. Average transmitted power is given by
Rom
Py =
11. Duty cycle of radar is dependent on
i) Type of waveform if) Pulse wit
Mi pPviee coomeceniony iv) Radar range
  
  
   
 
  
 
@ scanned with OKEN ScannerSS verge transmitted power? How itafects radar range ?
cribe briefly range ambiguities in radar system.
various system losses in any radar.
 
death ca
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