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Radars and Meteorology
Shri S.H. Damle
Indian Institute of Tropical Meteorology
Pune
Radar & Meteorology
Historical Back Ground
Basic concept of Radar
Nikola Tesla – 1900
Article in Century Magazine
Some british & German Patents
on Detection & Ranging of
Remote metallic objects by
Radio Waves – 1900-1906
First practical Demonstration of
Ranging using FM-CW
transmitter.
Dec 1924
Appleton – Kings College London
Barnet - Cambridge University
 They observed the reflections from
ionospheric layers beyond 100 km –
The Appleton Layer
 Use of Pulsed Techniques:
Breit & Tuve – Carneigy Institute
1925, with NRL collaborations.
Again Inospheric Echoes – 150 km
away.
 Work in another direction was
being perused by a young engineer
turned Meteorologist (Sir)
Watson. Watt – 1915
 Study of e-m radiation by
lightening in thunderstorms
 Objective : Timely thunderstorm
warnings to world War I
aviations.
 1935 : World War II scenario
 British govt. committee on scientific
survey of Air Defence (CSSAD)
 Consultations with sir Watson Watt &
Wilkins
 Proposal firmed up – 27 Feb 1935
 Successful Demonstration of detection
& ranging of aircraft – July 1935.
 This early war time effort firmly
established that RADAR was a tool
of Aviation.
 Since it evolved through the effort
of meteorologists meteorology was
clubbed as part of civil Aviation.
Even in India – as in many other
countries Dept. of meteorology was
a part of Dept of civil Aviation
 1940 – Dr. J.W. Ryde work on a 10 cm
Radar – Most probably related to
precipitation detection; but no direct
record of the period – wartime
secrecy.
 1946 – Ryde’s publication on
estimation of attenuation and echoing
properties of clouds & rain.
 Thus 1940-46 may be marked as the
Birth of Radar Meteorology.
 Early Radars deployed in RADAR
Meteorology
 S & C Band 2700 MHz / 5600 MHz
 Most of these were pulsed incoherent
Radars – the Tx source being high power
Magnetrons
 These were suitable for receiving echoes
form precipitation/detecting,
cyclonic/severe weather system: mostly
Intensify/reflectivity estimations.
 Quantitative Estimation of wind fields
could only be done by scan to scan
tracking
 Reflectivity Mapping : DVIP
 The advent of Klystron Technology then
led to development of Doppler weather
Radars which could directly measure the
average wind speeds in the cyclonic
systems:
 The advances in digital/computational
Technology then gave further impetus to
these Radar system developments.
 The Polarization diversity Radar – An effort
to improve precipitation measurements by
weather Radars
**Hydrometeors/Raindrops tend to elongated
as they fall from height.
**The scattering x-sections in the two
polarizations is therefore different.
**The differential reflectivity in the two
polarizations give a better handle on rain rate
estimation.
**Typical dual polarization radar requires
polarization switching n a pulse to pulse basis
requiring advanced high power switching
technology.
The Clear air Radar – Wind profiler
 Gradients in refractive index
fluctuations leading to e-m back
scatter
 The average wind carries along these
irregularities and in turn they become
tracers of mean wind.
 A Radar operating at wavelength λ is
most sensitive to scale sizes of these
irregularities of λ/2 or multiples of λ/2.
 The atmospheric Radar Eqn – volume Target
Eqn : The signal power

















.
.
2
ln
64
,
4
.
.
4
.
2
ln
16
.
4
2
2
2
2
2
c
R
A
P
P
Thus
A
A
G
A
R
c
R
R
G
P
P
e
r
t
t
r
e
e
t
e
r
t
t
t
r













Note:
Dependence on 1/R2
Proportional to Ae PT : power
Aperture product
Proportional to - The Radar
pulse length
η: volume Reflectivity of
atmospheric Target

c
The Noise Power
In Practice:
• One integrates nc pulses – assuming the signal remain
coherent during the period - typically upto few
seconds in troposphere.
• Invariably use spectral processing to detect the signal
and use DFFT techniques with P points DFT
i) Integrate certain number (ni) of spectra ‘incoherently’
the delectability is then defined as (S/N)dt
   i
B
r
t
r
dt
n
m
P
nc
B
Ts
T
k
R
c
Ae
N
S .
.
.
)
(
2
ln
64
)
(
Pr
2














B
T
T
k
B
kT
P
N n
B
r
s
n )
( 


 
Coding & Decoding
 Coding offers dual advantages:
*Good/High resolution
*High average power
*A long single pulse made up of
segment of pulses
*Binary phase coding is one convenient
form of coding technique which is
suitable for digital implementation
 The carrier phase is altered either as
0o or 180o according to a binary code
 Complementary code sequences are
popular in profiler applications
 If A & B are two complementary
codes then they possess the property
that the range side lobes of
autocorrelation function of A are in
opposite sign to the autocorrelation
function of B.
Thus if the complementary
sequences A & B are transmitted
one after the other and on receive
side their autocorrelation
functions are added the range
side lobes disappear in the
receiver output leaving in the
receiver output a single peak at
signal location.
 Once we know A & B are
complementary codes, then &
are also complementary.
 Examples A ++ AB +++-
B +- AB ++-+
Use of ‘m’ baud complementary code
pair sequence, & subsequent
decoding & addition on receive side
thus provides a (S/N) improvement
by a factor m.
B
A
B
A
AB
 This is because all the target returned
energy which was distributed in range
side lobes is recovered & this is as if
Transmit power is increased ‘m’ times
compared to a single pulse (code)
transmission.
 In the Pune profiler a 8 baud code pair
sequence (baud length 2 microsecond)
is used in the higher height mode of
operation. The code pair is +++- ++-+
+++- --+-
which can be generated from the basic
pair ++ & +-
Receiver system ‘Hardware consideration’
Since Cn
2 in atmosphere could vary by more
than 70 dB ( 7 orders of magnitude) a high
dynamic range receiver is required.
 The signal dynamic range is to be achieved
without saturation of any stage because of
background noise.
 RF & video gain is to be adjusted such that
the lowest expected signal level at Rx input is
amplified upto atleast ‘one bit’ level of the
ADC.
 This will ensure full utilization of the DSPG
I-Q Imbalance
damle-lec.ppt
The basic vector wind computation
Vradial(east) = ucosθ + wsinθ
Vradial (north) = vcosθ + wsinθ
W (zenith) = w
U &V being Zonal and Meridional
component of the wind.
W Zenith beam estimate of vertical velocity.
Quality controls on data
 Range tracking; temporal continuity:
consensus averaging
 Need to know beam position angle θ
accurately.
 If u>>w
Vre = ucosθ therefore
Thus for 1% accuracy of radial wind
Is approximately .170 for θ~750

d
V
V
r
r
tan




d
Similar systems abroad
 NOAA Network at 449 MHz: Typical specs – identical with Pune
profiler-Summary performance
damle-lec.ppt
damle-lec.ppt
damle-lec.ppt
damle-lec.ppt
damle-lec.ppt
damle-lec.ppt

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damle-lec.ppt

  • 1. Radars and Meteorology Shri S.H. Damle Indian Institute of Tropical Meteorology Pune
  • 2. Radar & Meteorology Historical Back Ground Basic concept of Radar Nikola Tesla – 1900 Article in Century Magazine
  • 3. Some british & German Patents on Detection & Ranging of Remote metallic objects by Radio Waves – 1900-1906 First practical Demonstration of Ranging using FM-CW transmitter. Dec 1924 Appleton – Kings College London Barnet - Cambridge University
  • 4.  They observed the reflections from ionospheric layers beyond 100 km – The Appleton Layer  Use of Pulsed Techniques: Breit & Tuve – Carneigy Institute 1925, with NRL collaborations. Again Inospheric Echoes – 150 km away.
  • 5.  Work in another direction was being perused by a young engineer turned Meteorologist (Sir) Watson. Watt – 1915  Study of e-m radiation by lightening in thunderstorms  Objective : Timely thunderstorm warnings to world War I aviations.
  • 6.  1935 : World War II scenario  British govt. committee on scientific survey of Air Defence (CSSAD)  Consultations with sir Watson Watt & Wilkins  Proposal firmed up – 27 Feb 1935  Successful Demonstration of detection & ranging of aircraft – July 1935.
  • 7.  This early war time effort firmly established that RADAR was a tool of Aviation.  Since it evolved through the effort of meteorologists meteorology was clubbed as part of civil Aviation. Even in India – as in many other countries Dept. of meteorology was a part of Dept of civil Aviation
  • 8.  1940 – Dr. J.W. Ryde work on a 10 cm Radar – Most probably related to precipitation detection; but no direct record of the period – wartime secrecy.  1946 – Ryde’s publication on estimation of attenuation and echoing properties of clouds & rain.  Thus 1940-46 may be marked as the Birth of Radar Meteorology.
  • 9.  Early Radars deployed in RADAR Meteorology  S & C Band 2700 MHz / 5600 MHz  Most of these were pulsed incoherent Radars – the Tx source being high power Magnetrons  These were suitable for receiving echoes form precipitation/detecting, cyclonic/severe weather system: mostly Intensify/reflectivity estimations.
  • 10.  Quantitative Estimation of wind fields could only be done by scan to scan tracking  Reflectivity Mapping : DVIP  The advent of Klystron Technology then led to development of Doppler weather Radars which could directly measure the average wind speeds in the cyclonic systems:  The advances in digital/computational Technology then gave further impetus to these Radar system developments.
  • 11.  The Polarization diversity Radar – An effort to improve precipitation measurements by weather Radars **Hydrometeors/Raindrops tend to elongated as they fall from height. **The scattering x-sections in the two polarizations is therefore different. **The differential reflectivity in the two polarizations give a better handle on rain rate estimation. **Typical dual polarization radar requires polarization switching n a pulse to pulse basis requiring advanced high power switching technology.
  • 12. The Clear air Radar – Wind profiler  Gradients in refractive index fluctuations leading to e-m back scatter  The average wind carries along these irregularities and in turn they become tracers of mean wind.  A Radar operating at wavelength λ is most sensitive to scale sizes of these irregularities of λ/2 or multiples of λ/2.
  • 13.  The atmospheric Radar Eqn – volume Target Eqn : The signal power                  . . 2 ln 64 , 4 . . 4 . 2 ln 16 . 4 2 2 2 2 2 c R A P P Thus A A G A R c R R G P P e r t t r e e t e r t t t r             
  • 14. Note: Dependence on 1/R2 Proportional to Ae PT : power Aperture product Proportional to - The Radar pulse length η: volume Reflectivity of atmospheric Target  c
  • 15. The Noise Power In Practice: • One integrates nc pulses – assuming the signal remain coherent during the period - typically upto few seconds in troposphere. • Invariably use spectral processing to detect the signal and use DFFT techniques with P points DFT i) Integrate certain number (ni) of spectra ‘incoherently’ the delectability is then defined as (S/N)dt    i B r t r dt n m P nc B Ts T k R c Ae N S . . . ) ( 2 ln 64 ) ( Pr 2               B T T k B kT P N n B r s n ) (     
  • 16. Coding & Decoding  Coding offers dual advantages: *Good/High resolution *High average power *A long single pulse made up of segment of pulses *Binary phase coding is one convenient form of coding technique which is suitable for digital implementation
  • 17.  The carrier phase is altered either as 0o or 180o according to a binary code  Complementary code sequences are popular in profiler applications  If A & B are two complementary codes then they possess the property that the range side lobes of autocorrelation function of A are in opposite sign to the autocorrelation function of B.
  • 18. Thus if the complementary sequences A & B are transmitted one after the other and on receive side their autocorrelation functions are added the range side lobes disappear in the receiver output leaving in the receiver output a single peak at signal location.
  • 19.  Once we know A & B are complementary codes, then & are also complementary.  Examples A ++ AB +++- B +- AB ++-+ Use of ‘m’ baud complementary code pair sequence, & subsequent decoding & addition on receive side thus provides a (S/N) improvement by a factor m. B A B A AB
  • 20.  This is because all the target returned energy which was distributed in range side lobes is recovered & this is as if Transmit power is increased ‘m’ times compared to a single pulse (code) transmission.  In the Pune profiler a 8 baud code pair sequence (baud length 2 microsecond) is used in the higher height mode of operation. The code pair is +++- ++-+ +++- --+- which can be generated from the basic pair ++ & +-
  • 21. Receiver system ‘Hardware consideration’ Since Cn 2 in atmosphere could vary by more than 70 dB ( 7 orders of magnitude) a high dynamic range receiver is required.  The signal dynamic range is to be achieved without saturation of any stage because of background noise.  RF & video gain is to be adjusted such that the lowest expected signal level at Rx input is amplified upto atleast ‘one bit’ level of the ADC.  This will ensure full utilization of the DSPG
  • 24. The basic vector wind computation Vradial(east) = ucosθ + wsinθ Vradial (north) = vcosθ + wsinθ W (zenith) = w U &V being Zonal and Meridional component of the wind. W Zenith beam estimate of vertical velocity.
  • 25. Quality controls on data  Range tracking; temporal continuity: consensus averaging  Need to know beam position angle θ accurately.  If u>>w Vre = ucosθ therefore Thus for 1% accuracy of radial wind Is approximately .170 for θ~750  d V V r r tan     d
  • 26. Similar systems abroad  NOAA Network at 449 MHz: Typical specs – identical with Pune profiler-Summary performance