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1 Hankuk Aviation Univ.레이다 공학
Lecture 8 : Radar Transmitters and Antenna
Objective- 레이다 송신기의 구성과 원리 이해
- 송신기 종류에 따른 특성 이해
- 안테나의 원리와 종류에 따른 특성 이해
주요 내용- 8.1 Transmitter Introduction and Functions- 8.2 Klystron Transmitters- 8.3 Traveling Wave Tube (TWT) Transmitters- 8.4 Crossed-Field Amplifier (CFA) Transmitters- 8.5 Magnetron Transmitter- 8.6 Solid State Transmitter- 8.7 Modulator- 8.8 High-Voltage Power Supplies- 8.9 Transmitter Vacuum and Cooling Systems- 8.10 Transmitter Monitoring and Testing- 8.11 Transmitter Parameters- 8.12 Microwave Components- 8.13 Waveguide- 8.14 Radar Antenna- 8.15 Sidelobe Suppression Technique- 8.16 Reference
2 Hankuk Aviation Univ.레이다 공학
8.1 Transmitter Introduction and Functions
Radar Transmitter- Functions
generate the EM signal for target illumination.tow type : coherent amp & non-coherent amp
- Block Diagram
<Radar Transmitter Generic Diagram>
2
3 Hankuk Aviation Univ.레이다 공학
8.1 Transmitter Introduction and Functions
Transmitter Type
- O-type : linear beam - M/W amplifying tubes,klystrons,traveling wave tubes, twystrons
- M-type : crossed-field – M/W amplifying tubes, crossed-field amp(CFAs), magnetrons
- Solid-state m/w amp
4 Hankuk Aviation Univ.레이다 공학
8.1 Transmitter Introduction and Functions
Transmitter Characteristics
< Transmitter Characteristics >
3
5 Hankuk Aviation Univ.레이다 공학
M/W Tubes & ComponentsM/W tubes (8.2) Klystron transmitter.
(8.3) Traveling wave tube(TWT) transmitter.(8.4) Crossed-field amp(CFA) transmitter.(8.5) Magnetron transmitter.(8.6) Solid state transmitter.(8.7) Modulator.(8.8) High voltage power supplier.(8.9) Transmitter vacuum and cooling systems.(8.10) Transmitter Monitoring and testing.
M/W component (8.11) Duplexer, Signal limiter, Magic tee, Rotary joints,
isolator, Directional coupler. Wave guide ∝ freq. band
6 Hankuk Aviation Univ.레이다 공학
8.6 Solid State Transmitter
Characteristics- The advantages of solid-state devices over vacuum tubes are
well known and include lower voltage requirements and highreliability
- Their primary disadvantages are low power output per deviceand relatively poor operation at higher microwave frequencies
- Radar transmitters made up of solid-state devices are reservedfor the lower frequency bands and contain many devices operating in parallel
4
7 Hankuk Aviation Univ.레이다 공학
8.6 Solid State Transmitter
Many different types of solid state device- Bipolar junction transistors (BJTs)
conventional junction (NPN and PNP) transistors used primarilyas amplifiers
- Field-effect transistors (FETs)are primarily amplifiers
- Transferred-electron devices (TEDs) are forward-biased semiconductor devices
- Avalanche transit-time (ATT) devices are complex diodes operating in reverse breakdown
Solid-state devices can make up the entire transmitter in radars
8 Hankuk Aviation Univ.레이다 공학
8.6 Solid State Transmitter
Solid-state transmitter configurations
< Solid-State Transmitter Configurations >
5
9 Hankuk Aviation Univ.레이다 공학
8.6 Solid State Transmitter
The block diagram of a transmit/receive activearray module patterned after PAVE PAWS
< A Typical Transceiver Module (modeled after PAVE PAWS) >
10 Hankuk Aviation Univ.레이다 공학
8.10 Transmitter Monitoring and Testing
Test and Monitoring
< Typical Transmitter Test and Monitoring >
6
11 Hankuk Aviation Univ.레이다 공학
8.11 Transmit Parameter
Power- It is measured by sampling a fraction of the power output and
using an RF power meter
(dB)sensor meter theport to monitoring thefrom loss the L 3) Ch. sec - (dBfactor correction cycleduty the dccf
(dBm) readingmeter power (Average) the P (dBm)power speak r tranmitte the P
(dB)L dccf(dB) (dBm)P (dBm)P
C
M
T
CMT
====
++=
Frequency- It is made more difficult by pulsing
Counters : CW signals, the most accurate meterAbsorption wavemeters : Pulsed signals, less accurate,
harder to use than counter
12 Hankuk Aviation Univ.레이다 공학
8.11 Transmit Parameter
Pulse width and shape- Waveform monitors sample RF from the transmitter,
demodulate it, and display the envelope on an oscilloscope.One class of detector often used is square-law detector.
Spectrum- It tells much about how well the transmitter is operating- The spectrum depends on the wave being transmitted
(Hertz) lobe spectralmain theofbandwidth null-to-null : B (seconds) width pulseCW gated the:
2/B
N-N
N-N
ττ =
< Gated CW Spectra >
7
13 Hankuk Aviation Univ.레이다 공학
8.11 Transmit Parameter
VSWR and Return Loss- Reflections are measured using a dual directional coupler,
giving an attenuated sample of the forward power andsampling the reflected wave
|)| - (1 / |)| (1 voltageminimum / the voltagemaximum the
Ratio) WaveStanding (Voltage VSWR oltageincident v / the voltagereflected the t)Coefficienn (Reflectio
ΓΓ+==
−=Γ−
Transmitter, Modulator, and HVPS DC andPulse monitoring - Most transmitters have built-in test points to be used for
monitoring and testing DC and DC pulse voltages and currents
14 Hankuk Aviation Univ.레이다 공학
8.14 Radar Antennas
Parameters- Radiation pattern & directivity- Beamwidth & length efficiency- Aperture : effective area & efficiency- Gain & Efficiency.- Sidelobe definition & effects.- Field zones / Polarization
Functions- Act as a transducer & impedance match between Tx and
propagation-medium & between the medium and receiver- Provide gain & steer the Tx power to the desired angular
position
8
15 Hankuk Aviation Univ.레이다 공학
Radiation PatternRadiation pattern
2λ=lengthdipole
‧Communications
‧Secondary radar
‧ECM
‧Radar target
‧Clutter
‧Square of one-way pattern
(Gain 3dB B/W 6dB B/W)
(Sidelobe lower double)
16 Hankuk Aviation Univ.레이다 공학
Antenna Effective Length
( )antennaoflengtheffectiveDwhere
D
radiansD
eff
eff
effdB
=
⎟⎠⎞
⎜⎝⎛=
=
(deg)180
)(3
λπ
λθ
9
17 Hankuk Aviation Univ.레이다 공학
Effective Area & Beam Shape
( ) (deg)180,)(
,
)()(3
)()(3
)()()()()()(
πλθλθ
ηη
AZeffAZ
AZeffAZ
ELELLELeffAZAZLAZeff
DradiansD
DDDD
==
==
18 Hankuk Aviation Univ.레이다 공학
Antenna Sidelobe EffectSidelobes & sidelobe effects
대책 : Ultra low sidelobe ant.
sidelobe signal suppression tech.
SLB sidelobe blanking.
CSLC coherent sidelobe cancellation.
10
19 Hankuk Aviation Univ.레이다 공학
8.14 Radar Antennas
Antenna Field Zone- Flatness : for practical purpose,
less than of curvature.
-Fan field : longest distance to any point
on plane of ant.must be
less than
- Near field : range less than far field range.
16λ
16R λ+
48
16162
4
162
2
2
2
222
2
22
2
2
DR
RRRD
RRD
DRFF
=
++=+
⎟⎠⎞
⎜⎝⎛ +=+⎟
⎠⎞
⎜⎝⎛
=
λ
λλ
λλ
λ22DR =
< Near-and Far-Field Waves >
< Geometry for Solving Far-Field Distance >
20 Hankuk Aviation Univ.레이다 공학
8.14 Radar Antennas
Arrays of Discrete Elements- Arrays
Linear array – one element dimensionPlanar array – two element array dimensionConformal array- conforms to the shape of object(mounted the nose of a/c or missile)
- Array & continuous antenna - Same shape, D, area, illumination function, frequency- Element pacing < 2
λ
< Array/Continuous Antenna Equivalence >
11
21 Hankuk Aviation Univ.레이다 공학
8.14 Radar Antennas
- Beam pattern of array
< Array Multiplication Principle >
22 Hankuk Aviation Univ.레이다 공학
8.14 Radar AntennaRadar Antenna Configurations
<Radar Antenna Types>
12
23 Hankuk Aviation Univ.레이다 공학
8.14 Radar AntennaReflector Antennas
(a) Focal point feed reflector antenna- The focal point feed reflector antenna uses as a reflector a parabola of rotation with the feed at the paraboloid’s focus.
- Illumination is set by the feed antenna’s beam pattern only ->Difficult to control- Aperture blockage -> Depend on Feed and its supports
<Focal Point Feed Reflector Antenna>
24 Hankuk Aviation Univ.레이다 공학
8.14 Radar AntennaReflector Antennas
(b) Offset Feed Antenna- The offset feed reflector is a focal point feed antenna with part of - the reflector remove. - Purpose -> Reduce or eliminate aperture blockage- Illumination control -> Difficult
(c) Cassegrain Reflector Antenna- The cassegrain reflector system uses two reflectors, the primary being a parabloid and the secondary being an hyperboloid.
- Illumination control -> Difficult , Very large aperture blockage- The aperture Blockage -> Large
13
25 Hankuk Aviation Univ.레이다 공학
8.14 Radar Antennas
- Array of angular offset
< Array Beam Formation
- Equal Phase Element >
eistancdextraforphaseS
anglesteering
SS2pointnobservatiothetoarraytheofplanethefrom
elementadjacentbetweenestancdiindifferenceSr
:2
sin
sin360sin
:sin
πφΔλθ
θλ
θλπφΔ
θΔ
=
==
=
26 Hankuk Aviation Univ.레이다 공학
8.14 Phase-Steered ArrayElectronically Phase – Steered Arrays
ⓐ Conventional Array with Phase Shifter ⓑ Space-Fed Lens Array
ⓒ Reflector Array
14
27 Hankuk Aviation Univ.레이다 공학
8.15 Sidelobe Suppression TechniqueLow sidelobe antenna
- Illumination function -> Critical(Array antenna -> Good control of illumination)
- Aperture blockage -> Avoid
<Sidelobe Blanking Principle>
<Sidelobe Blanking System>
Sidelobe Blanking (SLB)
28 Hankuk Aviation Univ.레이다 공학
8.15 Sidelobe Suppression TechniqueCoherent Sidelobe Cancellation (CSLC)
<Coherent Sidelobe Cancellation Principle>
<CSLC System>
15
29 Hankuk Aviation Univ.레이다 공학
8.16 Reference[1] Radar Transmitters by G. W. Ewell, McGraw-Hill, 1981
[2] Microwave Tubes by A. S. Gilmour, Artech House, 1986
[3] Passive and Active Microwave Circuits by J. Helszajin, John Wiley & Sons, 1978
[4] Transmission Lines and Waveguide by L. V. Blake, John Wiley & Sons, 1969
[5] Antenna Engineering Handbook by R. C. Johnson and H. Jasik, McGraw-Hill, 1984
[6] Antenna Theory and Design by W. L. Stutzman and G. A. Thiele, John Wiley &Sons, 1981
[7] Aspects of Modern Radar by E. Brookner, Artech House, 1988
[8] Fields and Waves in Modern Radio by S. Ramo and J. R. Whinnery, John Wiley& Sons, 1953
30 Hankuk Aviation Univ.레이다 공학
Lecture 9 : Receiver & DisplayObjective - 레이다 수신기의 구성과 원리 이해- 수신기 종류에 따른 특성 이해- 디스플레이의 종류와 특성 이해
주요 내용- 9.1 Receiver- 9.2 Receiver Type- 9.3 RF Processor- 9.4 RF Attenuator & Filter , Amplifier- 9.5 Mixer- 9.6 Local oscillator- 9.7 AFC & COHO- 9.8 IF Amplifier- 9.9 Demodulator- 9.10 Radar Receiver Example- 9.11 Display- 9.12 Reference
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31 Hankuk Aviation Univ.레이다 공학
9.1 ReceiverReceiver
• GeneralRadar echo signal from antenna: -20dBm ~ -100dBm- very low amplitude of
for minimal detectable targetThus, its amplitude must be increased by the receiver amp.
<Basic Functional Receiver Block Diagram>
32 Hankuk Aviation Univ.레이다 공학
9.2 Receiver Type
<Crystal Video Receiver>
<Homodyne Receiver>
*Crystal Video Receiver- Early receiver type.- Amplified & immediately
converted to baseband freq.- Advantage : Simple
Inexpensive- Disadvantage : Overwhelming
standpoint*Homodyne Receiver- Amplified & immediately
converted in a mixer basebandfrequency
- Advantage : Simple- Disadvantage : Poor sensitivity
Inability, Difficult to suppressinterference
Receiver Type
17
33 Hankuk Aviation Univ.레이다 공학
9.2 Receiver Type - Superheterodyne Receiver
Superheterodyne Receiver
<Superheterodyne Receiver>
<Image-Reject Filter>
* Superheterodyne Receiver- Main signal amplification & filtering at an intermediate frequency
- Easier & better filter & amplifierdesign
- Advantage: Simply changing the frequency
* Image response-> Suppress for two reason
1) A second receiver bandwidth’sworth of noise (SNR reduce)
2) Another bandwidth(ECM-Image jamming)
34 Hankuk Aviation Univ.레이다 공학
9.2 Receiver Type - Superheterodyne ReceiverSuperheterodyne Receiver Type
<Double-Conversion Superheterodyne Receiver> <Triple-Conversion Superheterodyne Receiver>
Intermediate frequency -> too high -> Design of the IF amp. & filter is complicated-> For this reason, multiple-conversion superheterodyne receiver were
developed
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35 Hankuk Aviation Univ.레이다 공학
9.3 RF Processor
<RF Processor>
( / ) / at the input of sys( / ) / at the output of sys
S N in S NFS N out S N
= =
* Noise Figure / Noise Factor: noise figure is a measure of how much noise is added by the system
* Noise Figure (a) system temperature (b) Ant. Trans line(c) Receiver equivalent temp
RF Processor
36 Hankuk Aviation Univ.레이다 공학
Noise Factor of Multi-Stage Amplifier
The overall nose factor is
stagenththeofgaintheGstagenththeoffactornoisetheF
ratiopowerfactornoiseoveralltheFGGFGFFF
n
n
T
===
−+−+−+=)(
)110(....)]/()1[(]/)1[( 213121
<Noise Factor in Multi-Stage Amplifiers>
9.3 RF Processor
19
37 Hankuk Aviation Univ.레이다 공학
9.10 Radar Receiver Example
Search Receiver
<Search Receiver 1> <Search Receiver 2>
38 Hankuk Aviation Univ.레이다 공학
9.11 Radar DisplayRadar Display Summary
(1) A-scope : range vs amplitude(linear or log)(2) A/R scope : tracking radar(3) R-scope : tracking radar range gate
20
39 Hankuk Aviation Univ.레이다 공학
9.11 Radar Display – B Type
(4) B- scope : airborne, rectangular display target amplitude brightness of the spot.commonly used air-to-air combat display.
(5) B-Prime scope : az. vs closing velocity
40 Hankuk Aviation Univ.레이다 공학
9.11 Azimuth vs Elevation Display
(6) C- scope : rectangular or circular display(7) D- scope : azimuth vs elevation
F- scope : basically a tracking error scope
21
41 Hankuk Aviation Univ.레이다 공학
9.11 PPI & RHI
RHI(Range Height Indicator)
(8) PPI : Plan Position Indicator, or P-scope(9) RHI : Range-Height Indicator
42 Hankuk Aviation Univ.레이다 공학
9.12 Reference[1] J.B. Tsui, Microwave Receivers with Electronic Warfare Applications, New York
: Jonhn Wiley & Sons, 1986.
[2] S.J.Erst, Receiving System Design, Norwood MA : Artech House, 1984
[3] J.W.Taylor Jr., Ch.3 in M.I.Skolnik, Radar Handbook, 2nd ed., New York :: McGraw-Hill, 1990.
[4] S.Y.Liao,Microwave Devices and Circuits, Englewood Cliffs NJ : Prentice Hall, 1980
[5] J.W.Taylor, Jr.and J.Mattern, Ch.5 in M.I.Skolnik, Radar Handbook, 1st ed.,New York: McGraw-Hill, 1970.
[6] “IEEE Standard Radar Definitions,” IEEE Standard 686-82, New York : TheInstitute of Electrical and Electronics Engineers, 1982.