Date post: | 06-Feb-2018 |
Category: |
Documents |
Upload: | truongdiep |
View: | 216 times |
Download: | 0 times |
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
2013
Multi-antenna Array Measurements Using Digitizers
Presented by: Alexander Dickson, Agilent Technologies
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
2 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Multi-antenna Array Measurements
2
Agenda
โข Phased Array Applications Overview (10 min)
โ Antenna architectures and enabling technology
โ Benefits of modern phased array antennas
โ Test challenges of phased arrays
โข Testing Multi-Element Array Antennas(15 min)
โ Phase and gain measurements
โ Using complex signals
โ Sensitivity to match BW
โ Accelerate your measurements
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
3 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Multi-antenna Array Measurements
3
Agenda (cont.)
โข Configuring a Test System (10 min)
โ Phase coherence
โ Digitizer features
โ Conversion loss / NF, power levels
โ Occupied dynamic range
โ System-level calibration
โข Realized Solution (10 min)
โ M9703A digitizer
โ DDC and segmented memory
โ Measurement example
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
4 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Parabolic Dish
Antenna
Mechanically
Steered Array
Passive
Electronically
Scanned Array
Active
Electronically
Scanned Array
Antenna Architectures
APAR Marconi Martello S-723 AEGIS AN/SPY1D(V)
1940 - Cavity Magnetron
6-bit Digital Phase Shifter
4-bit Digital Phase Shifter
RADAR Dish Antenna
T/R Module Integrated Phase Shifters
T/R Modules
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
5 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Modern Active Electronically Scanned
Phased Array (AESA)
Key Benefits
โข Fixed position antenna
โข Ability to form multiple agile beams
โข Fast scan rates with hard to predict, irregular scan patterns
โข Independent transmit/receive modules per element
โข Reduced power loss from integration of RF source on each T/R
โข Graceful degradation โ single source failure will not cripple system
AESA Installed on First US Air Force F15C โ http://www.aviationnews.eu/
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
6 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Historical Phased Array Test Challenges
Aligning Radiating Elements for Optimum Performance
โข Phase and amplitude errors lead to an increase in side lobe levels (SLL)
โข Large side lobes indicate a waste of beam forming power and cause interference
โข Average side lobe level due to phase and amplitude errors (normalized to isotropic level and using ฮป/2 element spacing) [1]:
๐๐ฟ๐ฟ๐ = ๐ โ 2 + ๐ฟ2
โข Where โ is the phase error variance (radians) and ๐ฟ is the fractional amplitude error variance
SLL
-3dB
HP BW
[1]: J. Ruze, โPattern degradation
of space fed phased arrays,โ MIT
Lincoln Laboratory, Project Rept.
SBR-1, Dec. 1979.
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
7 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
New, or growing Challenges
โข Array Element Counts Increasing (need speed without loss of accuracy)
โข Digital Moving Closer to the Antenna (may not have access to stimulus in analog form)
โข Broadband Modulated Signals (not just pulsed) (need to generate and capture full-bandwidth signals)
โข Multi-Function (need flexible measurement system, other types of signal analysis such as modulation accuracy)
โ Search, SAR, etc.
โ Communications
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
8 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Multi-antenna Array Measurements
8
Agenda
โข Phased Array Applications Overview (10 min)
โ Antenna architectures and enabling technology
โ Benefits of modern phased array antennas
โ Test challenges of phased arrays
โข Testing Multi-Element Array Antennas(15 min)
โ Phase and gain measurements
โ Using complex signals
โ Sensitivity to match BW
โ Accelerate your measurements
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
9 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Two Approaches
โข Narrow Band Approach
โ Swept or stepped tone
โ Narrowband receiver
โ Measure one freq at a time
โ Cross-channel computations in time domain
โ Lower variance by integrating longer (narrower RBW)
โข Broadband Approach
โ Broadband stimulus
โ Wideband receiver
โ Measure all frequencies simultaneously
โ Compute cross-channel spectrum
โ Lower variance by averaging
Measuring Relative Phase and Gain
DUT RX +
DIGITIZER
Signal
Generator
AWG
Network Analyzers are limited to
narrowband measurements
Digitizers and VSAโs with DDCโs have
adjustable bandwidths
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
10 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Digital Down-conversion (DDC)
What is a digital down-converter?
Itโs a flexible processing block that allows an ADC to run at full rate while the
output sample rate and bandwidth are optimized to match the current signal.
โข Digital signal processing
โข Produces complex I&Q samples from real ADC samples
โข Frequency translation (tune)
โข Filter and decimation (zoom)
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
What a DDC Does For You:
โข Isolate the signal of interest
โข Improve the analog performance
and dynamic range (SNR, ENOB),
by reducing the amount of
integrated noise
โข Extend the amount of capture
memory (in seconds), or reduce the
amount of data that need to be
transferred for a given duration.
โข Reduce the workload on post-
processing algorithms less data
to analyze
11
DDC Benefits
Noise & other signals in the full ADC
BW are eliminated with DDC
Analyzed
bandwidth
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
12 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
DDC - Tune Result
12
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
13 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
DDC - Zoom Result
13
For a proper analytic signal,
the negative frequencies
need to be removed by the
decimation filters
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
14 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
DDC - Real vs. Complex
14
0 Hz f1 -f1
Bandwidth that determines sample rate
Real-Only signals are
conjugate symmetric about DC
Minimum sample rate: 2*f1
0 Hz
Complex signals can be
asymmetrical about DC
Minimum sample rate: B
Bandwidth that determines sample rate
B
B
2 Step Process
Tune (shift)
Zoom (filter and decimate)
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
DDC โ Process Gain for Measurements
15
DDC Bandwidth
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
16 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
DDC โ Noise Reduction in Time Domain
T0
System2
T0
System1
Phase measured
from reference
channel to other
channels
16
Decimation Ratio = 2
Decimation Ratio = 4
Decimation Ratio = 8
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
17 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Narrow-Band Computing Cross-Channel Time
Let r(t) be the reference channel and x(t) be the signal on one of the receive
channels. The test signal is positioned away from spurs and does not have to be at
the center of the IF.
Let X = [x0 x1 x2 โฆ xn-1 ] be N complex samples of x(t)
Let R = [r0 r1 r2 โฆ rn-1 ] be N complex samples of r(t)
In Matrix Form the complex number the can be converted to amplitude and phase is:
where Rโ is the conjugate transpose of R
In Summation Form the computation is:
๐ฎ๐ = ๐ ๐๐ป โ๐ ๐๐ป โ๐ตโ๐๐=๐
๐ ๐๐ป โ๐ ๐๐ป โ๐ตโ๐๐=๐
This calculation is unbiased as the expected value of
the noise and off-frequency spurious is zero
Use N=1 when the DDC bandwidth provides sufficient isolation from system spurs and integrated noise power.
Use N > 1, i.e. 10 or 100 samples, to reduce the phase variance due to noise and spurious.
๐ฎ๐ = ๐๐ โ
๐ ๐ โ
17
G1 = Complex ch-ch ratio (I&Q) Use this
to compute relative mag and phase
using:
Mag = ๐ผ๐(๐บ1)^2 + ๐ ๐(๐บ1)^2
Phase = tanโ1๐ผ๐(๐บ1)
๐ ๐(๐บ1)
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Frequency Domain Approach (wideband)
SX
SN
H(f) SY = HSX + SN
S x f( )
tx t( ) ej 2 f t
d
+
โข H(f) is DUT transfer function
โข x(t) is a broadband signal with energy at all frequencies of interest
(noise, chirp, etc.)
โข Sx is the vector input spectrum of x(t) computed as the FFT(x(t))
โข Sy is the vector output spectrum
โข Sn is noise
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Frequency Domain Approach (wideband)
SX
SN
H(f) SY = HSX + SN
S x f( )
tx t( ) ej 2 f t
d
Hest = GYX /GXX
GYX = SYSX *
GXX = SXSX*
* conjugate operation
+
Hest = SY /SX
Average operation
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
20 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Comparing Wide- and Narrow-Band
Response Methods
โข Narrowband is familiar (traditional network analysis, classic RADAR signal)
โข Tones used in narrowband have a 0dB peak/avg, with all of the source power at one frequency. May have better dynamic range.
โข Narrow RBWโs may have long settling times which slow measurements or degrade accuracy
โข Wideband signals can be almost anything provided thereโs energy at the frequencies of interest. May even be DUT generated. Can use chirps for 0dB pk/avg. Lower spectral power density than a tone.
โข Wideband signals that mimic DUT signals may be more DUT friendly, or provide a more realistic answer in the presence of nonlinearities. Pulse shaping, if present, doesnโt need to be gated.
โข For narrow RBWโs wideband measurements may be faster as all frequencies are captured in parallel. However, there are many variables such as data transfer time and number of averages that also need to be considered
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
21 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Agenda (cont.)
โข Configuring a Test System (10 min)
โ Phase coherence
โ Digitizer features
โ Conversion loss / NF, power levels
โ Occupied dynamic range
โ System-level calibration
โข Realized Solution (10 min)
โ M9703A digitizer
โ DDC and segmented memory
โ Measurement example
Multi-antenna Array Measurements
21
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Configuring a Test System
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
23 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Requirements for a Digitizer
Feature List:
โข Multi-channel (n inputs), where n >= antennas in a group
โข Sufficient 3dB analog BW
โข Digital down converter (DDC)
โข Phase coherent inputs (< 1 degree phase diff)
โข Scalable platform
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
24 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Requirements for RF Signal Chain
Signal Path Analysis
โข Cable losses along signal path (vary depending on frequency)
โข Cascaded Noise Figure (Friis)
โข Understand the SNR and absolute power level at digitizer input
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Two Methods Used:
โข Sine-fit
โ Mathematic sine fit to single tone samples
โ Based on IEEE basic test methods for digitizers
โ Relatively slow as compared to DDC
โข DDC (software)
โ Uses complex samples
โ Complex conjugate ratio method cancels common mode phase modulation
Measuring Digitizer Ch-Ch Phase Coherence
Signal Generator (CW)
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
26 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Measuring Digitizer Ch-Ch Phase Coherence
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
27 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
System Level Calibration
Considerations:
โข How accurate is good enough?
โข At what is your IF center frequency and IF BW?
โข Using the DDC?
โข Using one or more digitizers?
โข What software environment are you using?
โข Do you have data on complex frequency response for all signal path
blocks out to the calibration reference plane?
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
28 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
System Level Calibration (cont.)
Signal Source (Step
Generator, Comb
Generator) with
Known Complex
Frequency
Response
IF Magnitude and Phase Calibration with Channel Matching
Signal
Path
NF and Gain
Known (SP)
Digitizer
(ADC 1) Signal
Path
NF and Gain
Known (SP)
Digitizer
(ADC 1) Signal
Path
NF and Gain
Known (SP)
Digitizer
(ADC 1) Signal
Path
NF and Gain
Known (SP)
Digitizer
(ADC 1) Signal
Path
NF and Gain
Known (SP)
Digitizer
(ADC 1) Signal
Path
NF and Gain
Known (SP)
Digitizer
(ADC 1) Signal
Path
NF and Gain
Known (SP)
Digitizer
(ADC 1) Signal
Path
Response
Known (SP1)
Digitizer
(ADC 1) S
plit
ter
Convolution of response for source, signal path and digitizer is represented in
digitized waveform FFT (divide out source and signal path):
* W1 = Source * SP1 * Digitizer Response1
* Note: Need to account for splitter impact on ch-ch phase. Possibly using differential 2-step cal.
Digitized W1
Source
CH 1 CH 2
CH 3 CH 4
CH 5 โฆ
โฆ CH N
Cal Ref
Plane
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
29 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
System Level Calibration (cont.)
Magnitude Phase
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
30 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Agenda (cont.)
โข Configuring a Test System (10 min)
โ Phase coherence
โ Digitizer features
โ Conversion loss / NF, power levels
โ Occupied dynamic range
โ System-level calibration
โข Realized Solution (10 min)
โ M9703A digitizer
โ DDC and segmented memory
โ Measurement example
Multi-antenna Array Measurements
30
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
31 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Agilent M9703A High-Speed Digitizer
Key Features
โข 12 bit Resolution
โข 8 channels @ 1.6 GS/s
โข Interleaving option to get 4 ch @ 3.2 GS/s
โข DC to 2 GHz analog 3dB bandwidth
โข Optional real-time digital downconversion
(DDC) on 8 phase-coherent channels
โข Up to 256 MS/ch memory and segmented
acquisition
โข > 650 MB/s data transfer
โข Agilent 89600 Software support
Reduce the test time of your DUT with the new M9703A! Higher number of synchronous acquisition channels, wider signal capture with the
best accuracy and flexibility, and optimized throughput
M9703A OS support
โข Windows
โข XP (32-bit)
โข Vista (32/64-bit)
โข 7 (32/64-bit)
โข Linux
Drivers โ MD1 software
โข IVI-C, IVI-COM
โข LabVIEW
โข MATLAB (through IVI-COM)
OTS application software
โข MD1 soft front panel
โข AcqirisMAQS U1092A-S01/S02/S03
โข 89600 VSA software
31
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
32 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
x8
M9703A - DDC Features and Benefits
โข Reduce the bandwidth to match the signal
โ Reduce noise (including quantization noise) and interference,
โ Allows lower sample rate without aliasing
โข Reduce sample rate to the appropriate values for the signal being analyzed.
โ More efficient use of memory allows longer duration captures
โ Or, allows less data to transfer for the same duration
โข Baseband (0 Hz, real-only) or use LO (complex) to โtuneโ
32
Full Sample Rate
(1.6 GSa/sec)
Frequency
Shift
Decimation
Filter
Sample
Rate
Analysis
Bandwidth 1.6 GS/s 1 GHz
400 Ms/s 300 MHz
200 Ms/s 160 MHz
100 Ms/s 80 MHz
50 Ms/s 40 MHz
50/2N Ms/s 40/2N MHz
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Optimum Memory Utilization
โข Accelerate test time with fewer samples
โข Reduced acquisition cycle time
โข Longer duration acquisitions
M9703Aโs Segment Memory Mode
Event 1 Event 2 1 2
3
Segmented memory optimizes capture time by
dividing the digitizerโs available acquisition memory
into smaller segments.
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
AWG
Demo Setup
AWG Configured to Generate 100MHz Wide LFM Chirp
Digitizer Configured as a Multi-channel Tuned Receiver
Trigger
Signals here have bandwidthโฆ
And because they have BW, we can compute FRF at multiple frequencies.
Split
ter
RX +
DIGITIZER
PC w/
89600
VSA SW PCIe
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
The Hardware
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
36 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Broadband Stimulus Signals
Chirped Pulse (e.g. Radar)
Spectrum
PvT
FRF Mag
FRF Phase
Pulse Width: 4usec
BWโ 100 MHz
Uniform Window
Trigger Delay
250 avgs/sec Spectrum
PvT
FRF Mag
FRF Phase
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Customer Requirement:
Multi-antenna array measurements
Element to element phase alignment for narrowband
and wideband signals
Obtain down-converted IQ data for further analysis
Hardware/Software:
N6171A MATLAB software
Agilent M9703A High Speed Digitizer
Agilent M8190A Arbitrary Waveform Generator
Demonstration:
Configure M9703A and acquire baseband IQ signals
Calculate and visualize:
โ Signal phase of each of the first four channels of M9703A
โ Narrowband Signal: Cross Channel phase correlation
โ Wideband Signal: Frequency Response Function (FRF) magnitude
and phase of channels 2x1, 3x1, and 4x1
MATLAB Demo: M9703A Cross Channel Phase
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Measurement Throughput
Segment #1 Rearm
(DUT dependent switching
time โ 80us)
Segment #2โฆ Offload
Segment Intervals Rearm Time DUT
Time
Acquisition
Cycle
Time/Interval Speed
500 us 100 160 us
(1.56 MSa/s)
80 us 660 us 6.6 us 152k int/sec/ch or
1.2M meas/sec
500 us 100 80 us
(3.125 MSa/s)
80 us 580 us 5.8 us 172k int/sec/ch or
1.4M meas/sec
500 us 10 40 usec (6.25
MSa/s)
80 us 580 us 58 us 17.2k int/sec/ch or
138k meas/sec
Acquire: 100
intervals (tones) or
10 intervals
(broadband)
Acquire: 100
intervals (tones) or
10 intervals
(broadband)
PCIe
trig trig
Idle
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
39 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Estimating Cross Channel Phase Variance
Variance and Power are closely related. For small angles we can use the relationship ๐ฅ โ sin (๐ฅ)and we also recognize that not all of the noise power goes to changing angle, it also changes amplitude. For a single channel we can show that the angle variance is
๐๐๐๐๐๐ ๐ถโ๐๐๐๐๐ ๐ด๐๐๐๐ ๐๐๐๐๐๐๐๐ = 180
๐
2โ10โ๐๐๐ 10
2 Noise is complex: NR+ jNI
Noise Power: NR2+ NI
2
For a nominal angle of zero degrees, only
the imaginary element of the noise
contributes to the angular variance hence
the angular variance in radians is half the
normalized noise variance
NR
NI
๐ถ๐๐๐ ๐ ๐ถโ๐๐๐๐๐ ๐ด๐๐๐๐ ๐๐๐๐๐๐๐๐ = 180
๐
2
โ10
โ๐๐๐ _๐๐๐ผ๐10
2+10
โ๐๐๐ _๐ ๐ธ๐๐๐๐๐๐ธ10
2
Noise on each channel is uncorrelated so we can simply add the variances to get:
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
40 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
EXAMPLE (using only the digitizer noise)
DUT
SNR = SigLevel โ (Noise Density + 10 log10 (ENBW)) where ENBW ~= 1/T
M9703
Noise Figure ~30dB (1V range)
Ch1 (stim) chN (resp)
-10dBm -50dBm
๐ถ๐๐๐ ๐ ๐ถโ๐๐๐๐๐ ๐ด๐๐๐๐ ๐๐๐๐๐๐๐๐ = 180
๐
2
โ10
โ๐๐๐ _๐๐๐ผ๐10
2+10
โ๐๐๐ _๐ ๐ธ๐๐๐๐๐๐ธ10
2
Assume T= 100 usec
SNR_STIM = -10 โ (-174 + 30 + 10log10(1.0/100usec)) = 94 dB
SNR_RESP = -50 โ (-174 + 30 + 10log10(1.0/100usec)) = 54 dB
Angle Variance = 6.5 mDeg2 or equivalently a standard deviation of 0.08 degrees
ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
41 ยฉ 2013 Agilent Technologies
Aerospace & Defense Symposium
Summary and Conclusion
Using an Agilent M9703A digitizer with DDC in a solution for multi-
antenna array measurements provides the following benefits:
1) Multi-channel coherent measurement solution (< 1 deg)
2) Fast, adjustable BW measurements producing complex samples with just enough sample rate (reduced variance)
3) Integrated 89600 VSA control (w/ hardware DDC acceleration) to leverage wealth of existing, industry standardized measurements
For more information:
www.agilent.com/find/axie-antennatest