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TRANSCRIPT
Hugh Griffiths
THALES / Royal Academy of Engineering Chair of RF Sensors
University College London
President, IEEE Aerospace and Electronic Systems Society
Bistatic and Multistatic Radar
IEEE AESS Distinguished Lecture, ETH Zurich, 7 November 2013.
• A bit of history
• Bistatic radar fundamentals
• A bit more history
• Bistatic radar clutter
• Passive Bistatic Radar …
2
Outline
The first radar – Hülsmeyer, 1904
3
The first radar – Hülsmeyer, 1904
4
Painting by Roy Huxley
The Daventry Experiment: 26 February 1935
5
Neale, B.T., ‘CH – the First Operational Radar’, GEC Journal of Research, Vol. 3 No.2
pp73-83, 1985.
CHAIN HOME
6
• The Chain Home radar has been described as a ‘dead-end design’, but as a
system to deliver an air defence capability it was certainly very effective.
• There were four (later reduced to three) metal transmitter towers in a line,
and four wooden receiver towers arranged in a rhomboid pattern. The
transmitter produced floodlight illumination of approximately 100°
beamwidth from a ‘curtain’ of eight horizontally-polarised half-wave dipoles,
each with a tuned reflector element 0.18λ behind. The curtain included a
main array above a secondary ‘gapfiller’ array of four dipoles. The stations
could be tuned to four different bands in the range 20 MHz to 30 MHz. The
operator could switch between the two arrays as needed. The output stage
of the transmitters used special water-cooled tetrode valves built by
Metropolitan Vickers.
• The wooden towers for the receiving arrays were shorter, about 76 m tall.
Each wooden receiving tower initially featured three receiving antennas, in
the form of two dipoles arranged in a cross configuration, spaced up the
tower. Additional crossed dipoles would be fitted later in the War to deal with
German jamming.
Greg Goebel, The Wizard War: WW2 and the Origins of Radar, http://www.vectorsite.net/ttwiz.html
CHAIN HOME
7
In the autumn of 1922, A.H. Taylor and L.C. Young of the Naval Research
Laboratory in the USA demonstrated detection of a wooden ship using a CW
wave-interference radar, at a wavelength of 5 m.
In December 1924, Appleton and Barnett in the UK used an FM radar technique to
measure the height of the ionosphere, and the following year Breit and Tuve in the
USA used a pulsed radar for the same purpose.
The first detection of aircraft using the wave-interference effect was made in 1930
by L.A. Hyland of the Naval Research Laboratory in the USA.
More history …
8
Appleton, E.V. and Barnett, M.A.F., ‘On some direct evidence for downward atmospheric reflection of
electric rays’, Proc. Roy. Soc., Vol.109, pp261-641, December 1925. (experiments at end of 1924)
ionosphere
transmitter
(Bournemouth)
receiver
(Oxford)
h
d
r
2
r dt
c
2 2 2
2
c t ctdh
The first FMCW radar
9
Freya,
Wassermann,
Mammut,
Jagdschloss –
early warning
Würzburg – fighter
control
Lichtenstein
SN2 – AI
German air defence radars
Bistatic radar - taxonomy
11
Bistatic radar
• bistatic radar has potential advantages in detection of targets which
are shaped to scatter energy in directions away from the
monostatic;
• the receiver is covert and therefore safer in many situations;
• countermeasures are difficult to deploy against bistatic radar;
• increasing use of systems based on autonomous air vehicles
(UAVs) makes bistatic systems attractive, since bistatic operation
may remove the need for a relatively small UAV to carry the heavy,
complex and power-hungry transmitter;
• many of the synchronisation and geolocation problems that were
previously very difficult are now readily soluble using GPS, and
• the extra degrees of freedom may make it easier to extract
information from bistatic clutter for remote sensing applications. 12
F-117A
13
TR
RR
transmitter receiver
Jackson, M.C., ‘The geometry of bistatic radar systems’; IEE Proc., Vol.133, Pt.F, No.7, pp604-612,
December 1986.
T
target
L
2 2
2 sin
T R
R
T R R
R R LR
R R L
2
baseline
extended
baseline
R
N
isorange contour
(ellipse)
T R
14
Bistatic radar geometry
Contours of constant bistatic range are ellipses, with the transmitter
and receiver as the two focal points
TR RR
+ = constT RR R
L = bistatic baseline
transmitter receiver
target
Targets lying on the transmitter-receiver baseline have zero bistatic range. 15
Bistatic radar geometry
This is derived in the same way as the monostatic radar equation :
The dynamic range of signals to be handled is reduced, because of the
defined minimum range.
TR RR
b
TG RG
2
2 2
0
2
3 2 2
0
1 1 . . . . .
4 4 4
4
R T T Rb p
N T R
T T R b p
T R
P P G GL
P R R kT BF
P G G L
R R kT BF
Bistatic radar equation
16
TP
transmitter receiver
Jackson, M.C., ‘The geometry of bistatic radar systems’; IEE Proc., Vol.133, Pt.F, No.7, pp604-612,
December 1986.
target
2
L
Rv
Tv
v
T
R
T
T R
Bistatic radar Doppler
17
2cos cos 2D
Vf For VT = VR = 0 ; V ≠ 0
special cases :
0
0
180
0
90
2
0,180
90 2
2 cos
Df
v
condition
monostatic
monostatic
forward scatter
v to bisector
v tx or rx
v bisector
v to tx or rx LOS
2v
0
0
22 cos 2v
2 cos 2v
sinv
Willis, N.J., ‘Bistatic radars and their third resurgence: passive coherent location’, IEEE Radar
Conference, Long Beach, USA, April 2002.
Bistatic radar Doppler
18
COMPLEX
TARGETS:
Assembly of discrete
scattering centers
Flat plates
Corner reflectors
Dihedrals
Resonant cavities
Ewell, G.W. and Zehner, S.P., ‘Bistatic radar cross section of ship targets’, IEEE J. Oceanic Engineering,
Vol.OE-5, No.4, pp211-215, October 1980.
Bistatic/Monostatic RCS ratios
for 4 small freighters
X-band, grazing incidence
19
Babinet’s principle tells us that we get exactly the same scattering from a
perfectly-absorbing target as we would from a target-shaped hole in an
infinite perfectly-conducting sheet !
0
20
Forward scatter
2
2
4b
A
(radians)B
d 2( )b
dBmB
10log f
30 MHz 100 MHz 300 MHz 1 GHz 3 GHz 10 GHz
20º
10º
0º
+60
+50
+40
+30
21
Forward scatter
Klein Heidelberg
22 Griffiths, H.D. and Willis, N.J., ‘Klein Heidelberg – the first modern bistatic radar system’, IEEE Trans.
Aerospace and Electronic Systems, Vol.46, No.4, pp1571–1588, October 2010.
Stellung BIBER
(Netherlands)
Stellung TAUSENDFÜSSLER
(Cherbourg)
Klein Heidelberg
23
picture © Jeroen Rijpsma
Klein Heidelberg
24
Klein Heidelberg
x
x
x
x
x x
Klein Heidelberg
BIBER
BIBER (Oostvoorne)
(Stellung BIBER, Oostvoorne) 30
Klein Heidelberg
L480 Bunker (Stellung BIBER, Oostvoorne)
Klein Heidelberg
31
Willis, N.J., ‘Bistatic Radar’, chapter 25 in Radar Handbook, second edition, (M.I. Skolnik ed.),
McGraw-Hill., 1990.
• All of the parameters
associated with
monostatic clutter –
plus geometry
• Little data exists
• Maximum at specular
reflection (‘specular
ridge’) and at forward
scatter
Bistatic radar clutter
32
Adapted from Willis, N.J., ‘Clutter’, chapter 9 in Bistatic Radar, Artech House, 1991
organization authors surface frequency polarization i s f
Ohio State
University
(1965)
Cost,
Peakes
smooth sand, loam,
soybeans; rough sand,
loam with stubble, grass
10 GHz VV, HH
HV
5 – 30˚
10 – 70˚
5 – 70˚
5 – 30˚
5 – 90˚
5 – 90˚
0 – 145˚
0, 180˚
0, 180˚
Johns Hopkins
University
(1966-67)
Pidgeon sea (sea states 1, 2, 3)
sea (Beaufort wind 5)
C-band,
X-band
VV, VH
HH
0.2 – 3˚
1 – 8˚
10 – 90˚
12 – 45˚
180˚
180˚
GEC Stanmore
(1967)
Domville rural land, urban land,
sea (20 kt wind)
X-band VV, HH 6 – 90˚
≈ 0 – 90˚
6 – 180˚
≈ 0 – 180˚
180, 165˚
180, 165˚
University of
Michigan
(ERIM) (1978)
Larson,
Heimiller
semidesert, grass with
cement taxiway, weeds
and scrub trees
1.3 and
9.4 GHz
HH, HV ≈ 0
10, 40˚
10, 15, 20 ˚
?
5, 10, 20˚
180, 165˚
0 – 180˚
0 – 105˚
Georgia
Institute of
Technology
(1982-84)
Ewell,
Zehner
sea (0.9, 1.2 – 1.8 m
wave heights)
9.38 GHz VV, HH ≈ 0 ≈ 0 90 – 160˚
University of
Michigan
(EECS) (1988)
Ulaby et
al.
smooth sand
rough sand
gravel
35 GHz
VV, HH
VH, HV
24˚
30˚
30˚
24˚
30˚
10 – 90˚
0 – 170˚
0 – 170˚
0 – 90˚
33
Bistatic radar clutter
Domville, A.R., ‘The bistatic reflection from land and sea of X-band radio waves’, GEC (Electronics) Ltd.,
Memo SLM 1802, Stanmore, England, July 1967.
In-plane, X-band
sea, horizontal
polarisation,
wind speed 20
knots
1 = 2 (monostatic)
grazing
incidence
normal
incidence
grazing
incidence
2 = 180 – 1 (specular)
34
Bistatic radar clutter
Bistatic angle ~50°
Yates, G.A., ‘Bistatic Synthetic Aperture Radar’, PhD thesis, University College London, January 2005.
Bistatic SAR image
35
Monostatic Bistatic
(~70°)
Yates, G.A., ‘Bistatic Synthetic Aperture Radar’, PhD thesis, University College London, January 2005. 36
Comparison of monostatic and
bistatic SAR image
It might be expected that bistatic clutter should be less ‘spiky’ since dihedral
and trihedral reflectors will not give strong reflections in bistatic geometries.
Very little experimental data exists – but results from bistatic imagery of urban
target scene show higher values of K-distribution shape parameter n for
bistatic geometry.
Yates, G.A., ‘Bistatic Synthetic Aperture Radar’, PhD thesis, University College London, January 2005.
monostatic bistatic
fit n fit n
field 1 16% 4.27 80% 10.01
field 2 72% 6.02 58% 6.25
field 3 46% 4.10 44% 5.64
37
Bistatic radar clutter
Carrier frequency 2.4 GHz
Peak transmitted power +23 dBm
Maximum range over which data is
recorded 3000 m
Antenna beamwidth 8º × 8º
Maximum bandwidth 50 MHz
Nominal range resolution 3 m
Pulse lengths 0.1 – 10 µs
Available transmissions Chirp, Barker code, Pulse, Polyphase /
Deng codes, Passive, Continuous
PRF 50 Hz – 3 kHz
Maximum number of pulses 1500
The current radar network consists of three nodes where two nodes are connected to a
central node with 50 m network cables.
A 100 MHz reference oscillator is also distributed to all three nodes via three 50 m cables.
The user interface to the system is by a PC connected via parallel port to the DSP card.
When outdoors, the system is powered by 65 Ah lead-acid battery.
38
NetRAD – a multistatic radar system
• September / October 2010, with support from ONR
Global, THALES UK and THALES NL
• In the Cape area of South Africa, in collaboration with
the University of Cape Town and CSIR
• Preceded by trials in the UK to prove correct operation
of the system and to gain experience
• A range of experimental parameters.
Bistatic clutter trials
39
40
Why South Africa ?
41
Bistatic clutter trials, Cape Point
Bistatic clutter trials, Cape Point
42
transmitter/
receiver
receiver
Bistatic clutter trials, Scarborough
transmitter/
receiver
receiver
Bistatic clutter trials, Scarborough
transmitter/
receiver
receiver
Bistatic clutter trials, Scarborough
Parameter Monostatic Node Bistatic Node
Carrier Frequency 2.4 GHz 2.4 GHz
Nominal Bandwidth 50 MHz 50 MHz
Beamwidth 9° (az) × 11° (el) 9° (az) × 11° (el)
Height above sea level 12 m 10 m
Rx losses and Noise Figure 7.7 dB 5.4 dB
Tx losses 2 dB -
Transmitted Power 500 W -
PRF 1 kHz -
• significant wave height 1.3 m
• swell propagating towards shore,
• sea state 2/3
• wind speed approximately 4 ms1
from a southerly direction.
1
0
expexpC N
n n
bxb x IP I dx
x p x p
n n
n
K+noise distribution:
V-pol clutter measurements, 5 October 2010
46
V-pol clutter measurements, 5 October 2010
47
RM m β σ0M dB m2/m2 σ0
B dB m2/m2 CNRM dB CNRB dB nM nB
805 30° 59.2 58.7 18.1 21.5 0.93 3.11
417 60° 47.1 47.6 36.9 40.2 0.22 0.48
295 90° 44.1 55.8 41.1 35.6 0.17 1.04
V-pol clutter measurements, 5 October 2010
48
clutter+noise
T
FA
V
P p R dR
p(R)
V T
monostatic
p(R)
V T
bistatic
R
R
A CFAR algorithm will set a
detection threshold to give a
particular value of PFA on the basis
of clutter+noise.
If the pdf of clutter+noise is shorter-
tailed, the detection threshold for a
given value of PFA will be lower.
Impact on detection performance
49
Bistatic target measurements: Simon’s Town (ii) Bistatic target measurements: Simon’s Town
transmitter/
receiver
receiver
50
Bistatic intensity plot and Doppler signature of a RHIB making two concentric circles. Bistatic angle~6o.
Target bistatic signatures
51
Time (s)
Do
pp
ler
(Hz)
Time-Varying Doppler Signature
0 20 40 60 80 100 120 -500
-400
-300
-200
-100
0
100
200
300
400
500
e10_10_16_1800_40_P1_1_130000_S0_1_2047_node3 - Node 3 Rx
RHIB target making circling manoeuvre 52
Target bistatic signatures
• NetRAD is a unique and highly flexible sensor which allows
measurements of bistatic radar clutter, bistatic target signatures and
experiments with networked radar
• Two sets of simultaneous measurements of monostatic and bistatic
sea clutter have shown that the shape parameter n of the K-distribution
is higher for the bistatic clutter – i.e. that the bistatic clutter is less
spiky.
• This may have important implications for the detection of small targets
against sea clutter
• Interesting measurements of bistatic signatures of maritime targets and
their wakes
• Lots more data, and lots more to do to analyse and understand …
Summary
53
In general, bistatic radar systems will use dedicated radar transmitters with explicit control
over location, modulation, scan pattern, etc.
However, it is also possible to use other transmissions that just happen to be there. These
are known as illuminators of opportunity, and the technique is sometimes known as
passive bistatic radar (PBR), hitchhiking, parasitic radar or passive coherent location
(PCL)
Such transmissions may be other radars, or they may be communications, broadcast or
navigation signals. In these days of spectral congestion there are more and more such
transmissions, and they are often high-power and favourably sited.
They also allow use of parts of the spectrum (VHF, UHF, …) that are not normally available
for radar purposes – where there may be a counter-stealth advantage (in addition to the
potential counter-stealth advantage that comes from the bistatic geometry)
As well as that, no transmitting licence is needed
And the radar is potentially completely covert, so countermeasures against it may be very
difficult
Passive Bistatic Radar (PBR)
54
• plenty – for ATC, long range air defence, AEW, etc.
• in general will scan in azimuth – hence synchronization and pulse
chasing necessary
• waveform and F very favourable
Existing radars (terrestrial, naval, airborne ... )
55
• VHF (~100 MHz), bandwidth ~50 kHz (c/2B = 3000 m); typically 4
channels per transmitter covering 10 MHz total
• broadband FM
• highest power transmitters in UK are 250 kW EIRP; many others of
lower power
• 250 kW EIRP gives F = 57 dBW/m2 @ 100 km
• omnidirectional in azimuth; vertical-plane radiation pattern shaped to
avoid wasting power above horizontal
http://www.bbc.co.uk/reception/
FM radio
56
FM radio
UCL ENGINEERING
Change the world
• BBC Radio 4, 93.5 MHz,
Wrotham (Kent)
• aircraft target on approach to
Heathrow, crossing baseline
• receiver located so that direct
signal is weak, hence beat
between direct signal and
Doppler-shifted echo has
maximum modulation
• Doppler shift goes through
zero as target crosses
baseline
Heathrow
airport
VHF FM
transmitter
Wrotham
93.5 MHz
bistatic receiver
50 km
58
Forward scatter VHF FM
• UHF (~550 MHz), bandwidth of video modulation ~5.5 MHz
• highest power transmitters in UK are 1 MW EIRP; many others of
lower power
Emley Moor is the tallest television mast
in England. It has a height of 330 metres
and weighs 11,000 tonnes. Picture courtesy of Dr Stuart Anderson, DSTO
Terrestrial analogue TV
59
Terrestrial analogue TV
60
vision
carrier chrominance
subcarrier
analog
sound
carrier
2MHz/div
digital
sound
carrier
vestigial-sideband
amplitude modulation
digital
TV channel
6 MHz
6.225 MHz
8 MHz
0 7 -1.25
measured spectrum of
analogue (and digital) TV
signals
In the UK the PAL (Phase Alternating
Line) modulation format is used, in which
the video information is coded as two
interlaced scans of a total of 625 lines at
a frame rate of 50 Hz. The start of each
line is marked with a sync pulse, and the
total duration of each line is 64 ms. The
video information is modulation onto a
carrier as vestigial-sideband AM, coded
as luminance (Red + Green + Blue) and
two chrominance signals (Green – Blue)
and (Red – Blue). The two chrominance
subcarriers are in phase quadrature, so
that they can be separately recovered.
The sound information (including stereo
information) is frequency-modulated onto
a second carrier.
Terrestrial analogue TV
61
http://www.sitefinder.radio.gov.uk
Cellphone basestations
62
• each consists of a network of 24
satellites; orbit height ~20,000 km
• both systems L-band (1200 – 1600
MHz)
• GPS is CDMA, GLONASS is FDMA
• bandwidths between 1 MHz and 10
MHz
• F = 134 dBW/m2 on ground
• timing and synchronisation not a
problem !
• claimed 60 – 70 dB processing gain
(1 Hz b/w)
He, X., Cherniakov, M. and Zeng, T., ‘Signal detectability in SS-BSAR with GNSS non-cooperative transmitters’; Special
Issue of IEE Proc. Radar, Sonar and Navigation on Passive Radar Systems, Vol.152, No.3, pp124–132, June 2005. 63
GPS / GLONASS / GALILEO
WiFi and WiMAX
64
WiFi WiMAX
K. Chetty, K. Woodbridge, Guo, Hui and G.E. Smith, ‘Passive bistatic WiMAX radar for marine surveillance’, Proc. IEEE
International Radar Conference RADAR 2010, Washington DC, 10–14 May 2010.
Guo, Hui, S. Coetzee, D. Mason, K. Woodbridge and C.J. Baker, ‘Passive radar detection using wireless networks’, Proc.
IET International Radar Conference RADAR 2007, Edinburgh, pp1–4, September 2007.
F (dBW/m2)
-50
-60
-70
-80
-90
-100
-110
-120
-130
-140
terrestrial TV @ 100 km
FM radio @ 100 km ENVISAT ASAR
satellite RA
cellphone basestation @ 10km
satellite DBS TV
satcoms
GPS / GLONASS / GALILEO
calculated on the
basis of a single
channel, free space
propagation, whole
signal, no processing
gain
WiFi @ 100 m
WiMAX @ 10 km
65
Comparison of power densities
85 dB
–50
–60
–70
–80
–90
–100
–110
–120
Pn = kT0BF = –122 dBm in B = 50 kHz 95 MHz 100 MHz
–40
–50
–60
–70
–80
–90
–100
–110
95 MHz 100 MHz
Noise levels in a passive radar receiver in FM radio band: (i) thermal noise in 50 kHz
bandwidth corresponding to 5 dB receiver noise figure; top of screen = –50 dBm (ii) signal
and noise levels measured from 10th floor of UCL in Central London on vertically-polarised
dipole antenna; top of screen = –40 dBm.
Noise level
66
FM Transmitter
Rx Tx
67
• 50 km from
receiver
• Height 375 m
• ERP 50 kW
• 96.8 MHz
• V-pol.
FM Radio Bistatic Radar
• Installed May 2002
$20 Reference Antenna
Surveillance Antenna
Digital V/UHF Receivers
68
Example Tracks
(4 second update rate using 1 PC)
150km
Phase interferometry used to estimate bearing – still needs calibration
69
70
Lockheed Martin Proprietary Information, Public Release – LM-MS Export/Import – 26 June 03
Silent Sentry Overview
Silent Sentry’s Passive Coherent Location (PCL) technologies enable
cost-effective, all-weather, persistent passive detection and tracking for
air surveillance and missile targets.
71
Lockheed Martin Proprietary Information, Public Release – LM-MS Export/Import – 26 June 03
NASA Phase 2.3, Fall 2002
KSC
Flagler Co
Airport
Vero
Beach
• Real-time Networked Operation
of 3 Silent Sentry Nodes
• Space Launch Vehicle Tracking
• STS-113
• Delta IV
• Atlas 2A
Historical Event – First EVER Real-Time, 3-D Space Launch
Vehicle Tracking using Indigenous FM Illuminators
73
Tracking of a Cessna 172 light aircraft using FM radio transmission
Courtesy of Craig Tong and Professor Mike Inggs,
University of Cape Town
74
PBR with an aircraft-borne receiver
75
PBR with an aircraft-borne receiver
Willis, N.J. and Griffiths,
H.D. (eds),
Advances in Bistatic Radar
A sequel to Willis, N.J., Bistatic Radar, Artech House,
1991
covering advances in the subject since 1991, and including recently-
declassified information on bistatic radar systems from previous decades,
as well as significant new material on passive bistatic radar.
76
Welcome !
Acknowledgements
Prof. DEN Davies, Dr John Forrest, Dr Jim Schoenenberger (formerly UCL)
Prof. Chris Baker (Ohio State University)
Prof. Ken Milne, Prof. Roger Voles, Prof. Ralph Benjamin, Dr Karl Woodbridge, Dr Alessio Balleri (UCL)
Dr Waddah Al-Ashwal (formerly UCL)
Prof. Mike Inggs, Stephan Sandenbergh (University of Cape Town)
Prof. Simon Watts, Dr Andy Stove (Thales Defence Systems)
Prof. Aaron Lanterman (Georgia Tech)
Tony Andrews (SAIC)
Dr Paul Howland, Darek Maksimiuk (NATO C3 Agency, The Hague)
Marc Lesturgie, Dominique Poullin, Pascale Dubois-Fernandez (ONERA, France)
Dr Chris Pell (formerly UK Ministry of Defence)
Dr Richard White, Michael Dunsmore, Dr Gill Yates (formerly DERA Malvern)
Dr Phil Judkins (Cranfield University)
Col. Michael Svejgaard
78