pulse radars transmit a burst of energy and listen for echoes between transmissions. leakage from...
TRANSCRIPT
Pulse radars transmit a burst of energy and listen for echoes between transmissions.
Leakage from the transmitterVery strong echoes from close-range clutter
Radar Receiver
The received signal is usually heavily corrupted by:
• Environmental noise• Interference• Noise from the radar system itself
Not occur at the receiving time
InputOutput
External Noise
Signal Receiver Noise
Receiver
Low
Output S/N
High
Input S/N
General pulsed Radar System Block Diagram
Receiver Components
Antenna: Some radar antennas include low-noise amplifiers prior to forming the receive beams
DuplexerPermits a single antenna to be shared between transmitter and
receiver.RF Filters
The receiver filters the signal to separate desired echoes from interference
Low Noise Amplifiers
Amplify the weak echo with minimum added noiseMixer
Down conversion
Oscillator
The radar front end consists of:Bandpass filter or bandpass amplifierLNADownconverter
Receiver Front End
Protection components
Protect the receiver from high power transmitter
The mixer itself and the preceding circuits are generally relatively broadband.
Tuning of the receiver, between the limits set by the preselector or mixer bandwidth, is accomplished by changing the LO frequency
LNAMixer
LO
Filter
IF
At IF:Amplification less costlyMore stable than at microwave frequencySimple filter operation
Superheterodyne principle is commonly used in radar receiver
More than one conversion step may be necessary to reach the final IF
IF range ( 0.1 and 100 MHz) without encountering serious image- or spurious-frequency problems in the mixing process.
Mixer
LO1
IF1RF
These advantages have been sufficiently powerful that competitive forms of receivers have virtually disappeared; only the superheterodyne receiver will be discussed in any detail.
IFIF-AmpMixer
LO2
Filter
IF2
The function of a radar receiver is to amplify the echoes of the radar transmission and to filter them in a manner that will provide the maximum discrimination between desired echoes and undesired interference.
The interference comprises:
• Energy received from galactic sources• Energy received from neighboring radars• Energy received from neighboring communication systems• Energy received from possibly jammers• Noise generated in the radar receiver • The portion of the radar's own radiated energy that is scattered
by undesired targets (such as rain, snow, birds, and atmospheric perturbations)
Receiver Function
In airborne radars are used for altimeters or mapping:
• Ground is the desired target
• Other aircraft are undesired targets
More commonly, radars are intended for detection of• Aircraft• Ships• Surface vehicles
Effect of Characteristics on Performance
Noncoherent pulse radar performance is affected by front-end characteristics in three ways:
1. Noise introduced by the front end restricts the maximum range. 2. Front-end saturation on strong signals may limit the minimum
range of the system or the ability to handle strong interference. 3. Finally, the front-end spurious characteristic affects the
susceptibility of off-frequency interference.
Coherent radar performance: Affected by spurious mixer characteristics:1- Range and velocity accuracy is degraded in the pulse doppler
radar2- Stationary-target cancellation is impaired in MTI (moving-target
indication) radar3- Range sidelobes are raised in high-resolution pulse
compression systems.
Vital receiver parameters:
1. Noise Figure or Noise temperature2. Dynamic range 3. Instantaneous bandwidth and tuning range4. Phase and amplitude stability5. Cooling requirements
Generally, the critical response is determined in the IF portion of the receiver
However, one cannot ignore the RF portion of the receiver merely by making it have wide bandwidth.
1- Paralyzing the receiver from reception (during transmission) 2- Protected from high power (burn out the input stage)
In low-power radars PIN diode switch can be used
More powerful modern radars may have twin PIN diodes, tuned respectively to magnetron frequency and magnetron principal spurious output frequency
Components of the radar receiver can cause degradation of the radiated transmitter spectrum?
Receiver protection
Magnetron
Circulator
Gas protection section
To antenna
High power Receiver protection
Waveguide a centimeter or so long, sealed by quartz windows at its ends and containing a 'gas' of particularly short de-ionisation time (~2 s), such as water vapour at absolute pressure ~ 0.O1 bar. After the transmission, the gas takes a few microseconds to de-ionise,
Components of the radar receiver can cause degradation of theradiated transmitter spectrum, generating harmonics of the carrier frequency or spurious doppler spectra, both of which are often required to be 50 dB or more below the carrier. Harmonics can create interference in other electronic equipment, and their maximum levels are specified by the National Telecommunications and Information Administration (NTIA) and MILSTD-469. Spurious doppler spectra levels are dictated by requirements to suppress clutter interference through doppler filtering.
Harmonics are generated by any component which is nonlinear at the power level created by the transmitter and which passes those harmonics to the antenna. Gaseous or diode receiver-protectors are designed to be nonlinear during the transmitted pulse and reflect the incident energy back toward the antenna.Isolators or circulators are often employed to absorb most of the reflected fundamental, but they are generally much less effective at the harmonics. Moreover, these ferrite devices are nonlinear in themselves and can generate harmonics.
Noise and Dynamic Range Considerations
The receiver is often the most critical component
The purpose of a receiver is reliably recovering the desired echoes from a wide spectrum of transmitting sources, interference and noise
Noise is added into an RF or IF passband and degrades system sensitivity
Receiver should not be overloaded by strong signals
Receivers generate internal noise which masks weak echoes being received from the radar transmissions. This noise is one of the fundamental limitations on the radar range
Noise
(So/No)min
ReceiverTo demodulator Desired echo + Noise
Internal NoiseDesired echo
Noise ultimately determines the threshold for the minimum echo level that can be reliably detected by a receiver.
The receiving system does not register the difference between signal power and noise power. The external source, an antenna, will deliver both signal power and noise power to receiver. The system will add noise of its own to the input signal, then amplify the total package by the power gain
Noise behaves just like any other signal a system processes
Filters: will filter noise
Attenuators: will attenuate noise
Noise Effects
Thermal NoiseThe most basic type of noise being caused by thermal vibration of bound charges. Also known as Johnson or Nyquist noise.
R
T Vn = 4KTBR
R
Available noise power Pn = KTB
Where, K = Boltzmann’s constant (1.3810-23J/K)
T Absolute temperature in degrees Kelvin
B IF Band width in Hz
At room temperature 290 K:
For 1 Hz band width, Pn = -174 dBm
For 1 MHz Bandwidth Pn = -114 dBm
Shot Noise:
Source: random motion of charge carriers in electron tubes or solid state devices.
Noise in this case will be properly analyzed on based on noise figure or equivalent noise temperature
Generation-recombination noise:
Recombination noise is the random generation and recombination of holes and electrons inside the active devices due to thermal effects. When a hole and electron combine, they create a small current spike.
Antenna Noise
In a receiving system, antenna positioned to collect electromagnetic waves. Some of these waves will be the signals we are interested and some will be noise at the same frequency of the received signal. So filters could not be used to remove such noise.Antenna noise comes from the environment into which the antenna is looking. The noise power at the output of the antenna is equal to KTaB. Ta is the antenna temperature. The physical temperature of the antenna does not influence the value of Ta.
The noise temperature of the antenna can be reduced by repositioning it with respect to sources of external noise
Assumptions
■ Antenna has no earth-looking sidelobes or a backtobe (zero ground noise)
■ Antenna is lossless ■ h is antenna elevation angle (degrees)
■ Sun not considered ■ Cool. temperate-zone troposphere
The background noise temperature increases as the antenna is pointed toward the horizon because of the greater thickness of the atmosphere. Pointing the antenna toward the ground further increas the effective loss, and hence the noise temperature.
At 22 GHz Resonance of molecular water At 60 GHz
Resonance of molecular oxygen
22 GHz 60 GHz
Equivalent Noise Temperature and Noise Figure
F = (S/N)i/(S/N)o
Ni = Noise power from a matched load at To = 290 K;
Ni = KTo B.
F is usually expressed in dB
F(dB)=10 log F.
Noise Figure (F)
Two-portNetworkSi + Ni So + No
Te = No/KB,
B is generally the bandwidth of the component or system
R No
white noise
source R R
Te No
Equivalent Noise Temperature (Te)
If an arbitrary noise source is white, so that its power spectral density is not a function of frequency, it can be modeled as equivalent thermal noise source and characterized by Te.
R
No
G
Noisy amplifier
T = 0
R R
No-int= GKTeBG
Noiseless amplifier
R
No-int
GKBTe =
Te ≥ 0
If To is the actual temperature at the input port, usually 290 K
Te may be greater or less than 290 K
Te = To( F – 1) F = 1 + TeTo
Output Noise due to the internal noise of the receiver
No = No-int + No-in
FGKToB = GKTeB + KToBG
Examples:
(1) the noise power of a bipolar transistor at 3 GHz is 0.001 pW for a 1-MHz bandwidth. What is the noise temperature?
Solution WN = KTB, T = WN/KB = 72.5 K ( ~ -217o
C)
F of the transistor is 0.97 dB
(2) the noise power of a mixer at 20 GHz is 0.01 pW for a 1 MHz bandwidth. what is the noise temperature ?
Solution WN = KTB, T = WN/KB = 725 K (435oC)
F = 5.44 dB
Noise Figure of Cascaded Components
Te = To (F - 1)
Ts = Ta + Te Pn = KTsBG,
where, G is the overall gain of the system = G1×G2×G3……×Gn
F2 – 1
G1
F3 – 1
G1 G2
Fn – 1
G1 G2 ….. Gn-1
FT = F1 + + + …… +
F1
G1
F2
G2
FN-1
GN-1
FN
GN
Noise Figure of Passive and Active Circuits
Passive Components:
For Matching component:
F = L (L Insertion Loss)
Te = To (L-1)
F Increases if the component is mismatched.
Active Devices:
It is generally easier and more accurate to find the noise characteristics by direct measurement
Conversion Noise
Noise Free signal and Local Oscillator:
-10 dBm
-130 dBm
-17.5 dBm
-130 dBm
IL=7.5 dBF=7.5 dB
LO
RFIF
KTB = -130 dBm
17 dBm
-130 dBm
Noise Figure = conversion loss
Noisy received signal & Noise free local oscillator
17 dBm
-130 dBm
-17.5 dBm
-97.5 dBm
IL=7.5 dBF=7.5 dB
-10 dBm
-90 dBm
-130 dBmLO
RF IF
Noisy Local Oscillator & Noise free input signal
-10 dBm
-130 dBm
IL=7.5 dBF=7.5 dB -17.5 dBm
-97.5 dBm
-130 dBm
17 dBm
-63 dBm
LO
RFIF
Noise Figure = 40 dB
80 dB
80 dB120 dB
Example: FT? Ts ? No ? Given IF bandwidth = 10 MHz
Noise
LNAMixer
LO
BPF
G = 10 dB
Ta = 15 KF = 2 dBL = 1 dB
L = 3 dBF = 4 dB
So , No
Si , Ni
1) dB to numerical valuesLNA G = 10 dB (10) BPF: G = -1 dB (0.79) Mixer: G = -3 dB (0.5)
F = 2 dB (1.58) F = 1 dB (1.26) F = 4 dB (2.51)
2) FT = [ 1.58 + 0.26/10 + 1.51 /7.9] = 1.8 (2.55 dB)
3) Te = To(F-1) = 290 (1.8 – 1) = 232 K
4) Ts = Ta + Te = 247 K5) No = KTsBG,
G is the overall Gain = G1×G2×G3×…. =10 × 0.79 × 0.5 = 3.95 (~6dB)
No = -98.7 dBm
Signal
The range of signal strength where the receiver will perform as expected
1. Minimum signal of interest: The input signal that produces unity signal-to-noise ratio (SNR) at the receiver output (minimum-detectable-signal).
2. Allowable deviation from expected characteristic: The maximum signal is one that will cause some deviation from expected performance. Linear receivers usually specify a 1 dB decrease in incremental gain (the slope of the output versus- input curve).
3. Type of signal: Three types of signals are of general interest in determiningdynamic-range requirements: distributed targets, point targets, and wideband noise jamming. If the radar employs a phase-coded signal, the elements of the receiver preceding the decoder will not restrict the dynamic range of a point target as severely as they will distributed clutter; the bandwidth-time product of the coded pulse indicates the added dynamic range that the decoder will extract from point targets.
The dynamic range can be defined in terms of:
Dynamic range,
Dynamic Range (DR), and 1-dB Compression Point
The operating range for which a system has desirable characteristics
Input power
1 dB compression point
Output
power
1 dB
Dynamic range
Noise level
Noise floor
MDS
The receiver dynamic range depends on the noise characteristics of the receiver as well as the type of modulation being used , and the required S/N
DR = Maximum allowable signal│dBm – MDS│dBm dB
Noise
(So/No)min
Receiver
TeFG
To demodulatorSi & Ta
No = KBG(Ta +Te) So = G Si
B is the IF BW (set by the IF bandpass filter)
MDS = Simi n = = Somin No So
G G No min
Local Oscillator
The superheterodyne receiver utilizes one or more local oscillators and mixers to convert the echo to an intermediate frequency that is convenient for filtering and processing operations. The receiver can be tuned by changing the first LO frequency without disturbing the IF section of the receiver. Subsequent shifts in intermediate frequency are often accomplished within the receiver by additional LOs, generally of fixed frequency.
Pulse-amplifier transmitters also use these same LOs to generate the radar carrier with the required offset from the first local oscillator. Pulsed oscillator transmitters, with their independent "carrier" frequency, use automatic frequency control (AFC) to maintain the correct frequency separation between the carrier and first LO frequencies.
In many early radars, the only function of the local oscillators was conversion of the echo frequency to the correct intermediate frequency. The majority of modern radar systems, however, coherently process a series of echoes from a target. The local oscillators act essentially as a timing standard by which the echodelay is measured to extract range information, accurate to within a small fraction of a wavelength. The processing demands a high degree of phase stability throughout the radar.
The first local oscillator, generally referred to as a stable local oscillator (stalo), has a greater effect on processing performance than the transmitter. The final local oscillator, generally referred to as a coherent local oscillator (coho), is often utilized for introducing phase corrections which compensate for radar platform motion or transmitter phase variations.
Oscillators are characterized by the following parameters:
1) Frequency
2) Frequency stability:
- Frequency pushing (frequency change with poor supply
voltage or current)
- Frequency pulling (frequency change with load mismatch)
- Temperature stability
- Shock and vibration effect
3) Spurious Performance
4) Phase noise
5) Power and efficiency
6) Tuning: Mechanical, Electronically, Tuning sensitivity (Hz/V or Hz/ mA), Settling time (the time it takes to respond to frequency control
signal) Post-tuning drift (drift after the oscillator reaches its desired
frequency )
The phase noise is defined as the power in 1-Hz bandwidth at a frequency fm from the carrier, and measured in dB below the carrier power.
The phase noise of microwave oscillator is 60 to 120 dB below the carrier power.
Phase noise
0
Phase noise
(dB)
1 KHz1
KHz
Effect of Phase Noise on Receiver Performance
How much phase noise can be tolerated in a given system design ?
IFIF IF
Desired LO
Phase noise
Noisy LO
Desired signal
undesired signal
Transmitted signal
Main signal Noise sideband
40 dB
Received signal
Main signal Noise sideband
40 dB
AirplaneMountain
How phase noise affect false detection for radar applications
In many early radars, the only function of the local oscillators was conversion of the echo frequency to the correct intermediate frequency. The majority of modern radar systems, however, coherently process a series of echoes from a target. The local oscillators act essentially as a timing standard by which the echodelay is measured to extract range information, accurate to within a small fraction of a wavelength. The processing demands a high degree of phase stability throughout the radar.
The first local oscillator, generally referred to as a stable local oscillator (stalo), has a greater effect on processing performance than the transmitter. The final local oscillator, generally referred to as a coherent local oscillator (coho), is often utilized for introducing phase corrections which compensate for radar platform motion or transmitter phase variations.
Mixers
LO + SIFLO
S
LO
V
I
IsVB
Non-linear I-V Characteristics of a diode
Mixers use nonlinear device to achieve frequency conversion of an input signal.
The drawback of nonlinear devices are that they generate many LO harmonics, and mixing products other than the desired one.
V = (VLsin wLt + Vssin wst), the mixer current will be
I = f(V) = ao + a1 (VLsin wLt + Vssin wrt) + a2 (VLsin wLt + Vrsin wst)2 + ……. + an (VLsin wLt + Vrsin wst)n
The primary mixing products (wL ± ws) come from the second order term and are proportional to a2 in amplitude
The third and higher order terms generate products of the form nwL ± mws and higher oredr harmonics
I = f(V) = ao + a1V + a2V2 + ……. + anVn
Where V and I are the device voltage and current
Mixer parameters
Important parameters are:(1) Conversion gain or loss
The ratio of IF power to microwave signal power. Conversion losses ranges from 5-6 dB for a single diode mixer to 9-10 dB for a double balanced mixer.
(2) Noise figure The ratio of signal to noise at mixer input to signal to noise at
mixer output. The noise figure determines the low-level sensitivity of the mixer. For passive mixers, assuming the devices do not generate any internal noise, we can use the conversion loss as the noise figure. Sometimes we can add 0.5 dB for account of the internal noise generation. For active mixers the noise figure and conversion loss are independently related.
(3) SWR at LO and RF inputs The mismatch at LO and signal ports
(4) LO/RF IsolationIsolation between LO and RF ports
(5) Harmonic suppressionsuppression of LO and signal harmonics
(6) Dynamic range It is the range of input power over which mixer provides required performance. The largest signal that can be handled by the mixer is determined by the acceptable level of intermodulation product, and is often specified by the requirement that the intermod products be below the noise level.
(7) 1-dB Compression point The input 1-dB compression point of a mixer is typically 5-8 dB below the input LO power. The output 1-dB compression point of a mixer can be calculated as the input 1-dB compression point minus the conversion loss of the mixer, minus 1 dB.For Example,■ LO power = 13 dBm ■ Conversion Loss = 8 dB ■ Input 1dB Compression point = + 6 dBm ■ Output 1-dB Compression point = +6 -8 -1 = -3 dBm
(8) Intermodulation product The amount of third order distortion caused by the presence of a second received signal at the output port (2f2 –f1 ± fLO). These products are extremely important because they will always occur with closely spaced input frequencies
(9) Intercept point The point at which the fundamental response and
the third-order spurious response curves intersect. The higher the intercept the point, the better the third-order compression. The input third order intercept point of a mixer is typically 4-5 dB above the input LO power. The output third order intercept point can be calculated as the input third order intercept point minus the conversion loss of the mixer.
Microwave input power
IF output
power1 dB
Input dynamic range
1 dB compression point
dBmIntercept point
Noise level
outp
ut
dyn
amic
ran
geIntermodulation
The sensitivity of the mixer in dBm is defined as the weakest signal that can be detected by the mixer and is given by:
S = -114 + NF + 10 log BW
Where NF is the mixer noise figure, BW the bandwidth in MHz and –114 dBm is the thermal noise in 1 MHz bandwidth
Selection of IF frequency:
fIF = |fRF - fLO|
For lower side band selection
fLO = fRF + fIF
Frequency Conversion and Filtering
Large IF eases the cutoff requirements of the image filter
FIF > BRF/2 Image frequencies outside RF BW
IF < 100 MHz Low cost
fLO
fRF Image
IF IF
Gain Controlled Amplifiers
Sensitivity Time Control (STC) The search radar detects echoes of widely differing amplitudes, typically so great that the dynamic range of any fixed-gain receiver will be exceeded.
Differences in echo strength are caused by differences :• In radar cross sections• In meteorological conditions• In range (the effect of range on radar echo strength
overshadows the other causes)
Also, many radar receivers exhibit objectionable characteristics when signals exceed the available dynamic range.These effects are prevented by the technique of sensitivity time control, which causes the radar receiver sensitivity to vary with time in such a way that the amplified radar echo strength is independent of range.
Most modern radars generate STC waveforms digitally. The digital commands may be used directly by digital attenuators or converted to voltage or current for control of diode attenuators or variable-gain amplifiers.
Clutter Map Automatic Gain Control
In some radars, mountain clutter can create echoes which would exceed the dynamic range of the subsequent stages of the receiver (A/D converter, etc.) if the STC attenuation at that range allowsdetection of small aircraft. The spatial area occupied by such clutter is typically a very small fraction of the radar coverage; so AGC is sometimes considered as an alternative to either boosting the STC curve (a performance penalty affecting detectability of small aircraft in areas of weaker clutter or no clutter) or increasing the number of bits of the A/D converter and subsequent processing (an economic penalty).
Clutter map AGC is controlled by a digital map which measures the mean amplitude of the strongest clutter in each map cell of many scans and adds attenuation where necessary to keep the mean amplitude well below saturation.
Automatic Noise-level Control
AGC is widely employed to maintain a desired level of receiver noise at the A/D converter. Too little noise relative to the quantization increment of the A/D converter causes a loss in sensitivity; too much noise means a sacrifice of dynamic range. Samples of noise are taken at long range, often beyond the instrumented range of the radar (in dead time), to control the gain by means of a slow-reaction servo. If the radar has RF STC prior to any amplification, it can achieve meaningful dead time by switching in full attenuation.
IF Gain Control circuit
IF Amp
Demodulator
LPF
Variable gain amp/attenuator
IF Input
DC AmpDC Ref
AGC detector
Gain Controlled Distributed Between RF and IF
IFdetector
IF amplifierFilter LNA MixerFilter
LPF
Comparator