Reverberation Chambers for EM Applications
Christopher L. Holloway
John Ladbury, Galen Koepke, and Dave Hill National Institute of Standards and Technology Electromagnetics Division Boulder, Colorado 303-497-6184, email: holloway@boulder.nist.gov
Reverberation Chambers for EM Applications Christopher L. Holloway - - PowerPoint PPT Presentation
Reverberation Chambers for EM Applications Christopher L. Holloway John Ladbury, Galen Koepke, and Dave Hill National Institute of Standards and Technology Electromagnetics Division Boulder, Colorado 303-497-6184, email:
Christopher L. Holloway
John Ladbury, Galen Koepke, and Dave Hill National Institute of Standards and Technology Electromagnetics Division Boulder, Colorado 303-497-6184, email: holloway@boulder.nist.gov
Ambients Reflections Scanning Interference Positioning
High Frequencies Reflections Test Volume Positioning
Test Volume Uniformity Along Cell Positioning
Low Frequencies Reflections Positioning
The classic emissions test and standard limits (i.e, testing a product above a ground plane at a specified antenna separation and height) have their origins in interference problems with TV reception.
One problem with the emissions test standard is that it is based on an interference paradigm (interference to terrestrial broadcast TV) that is, in general, no longer valid nor realistic today. In a recent report, the FCC indicated that 85 % of US households receive their TV service from either cable, direct broadcast satellite (DBS), or other multichannel video programming distribution service, and that only a small fraction of US households receive their TV via direct terrestrial broadcast. Coupling to TV antennas designed to receive terrestrial broadcast may no longer be an issue.
interference have been introduced into the marketplace.
computers (PCs). Many different products containing microprocessors (e.g., TVs, VCRs, PCs, microwave ovens, cell phones, etc.) may be operating in the same room.
(e.g., cars and airplanes). The walls, ceiling, and floor of an office, a room, a car, or an airplane may or may not be highly conducting.
be quite different from emissions at an OATS. In fact, the environment may more likely behave as either a reverberation chamber or a free space environment.
today's electromagnetic environment?
Thorough, …
D-U-T Transmit Antenna Receive Antenna Probe(s)
Signal Generator Amplifier Directional coupler Power Meter(s) etc. Motor Control Control and Monitoring Instrumentation for Device-under-test Receive Instrumentation: Spectrum Analyzer Receiver, Scopes Probe System etc.
Locations in the chamber with very high field values Locations in the chamber with very low field values Frozen Food
In a metal box, the fields have well defined modal field distributions. Small changes in locations where very high field values occur Small changes in locations where very low field values occur
Large changes in locations where very high field values occur Large changes in locations where very low field values occur In fact, after one fan rotation, all locations in the chamber will have the same maxima and minima fields.
exposure
Calibrate and Initialize system Establish Fields in Chamber Measure response of EUT, probes, receive antenna, etc. Generate new environment i.e. move paddle move antennas change frequency, etc. END <N =N
In reverberation chambers you cannot hide emission problems. Reverberation chambers will find problems.
200 400 600 800 1000
Frequency (MHz)
0.0E+0 1.0E-4 2.0E-4 3.0E-4 4.0E-4 5.0E-4 6.0E-4
| Emax | (V/ m) Class A: based on 10 m separation Class B: based on 3 m separation
by the device and/or product are below a maximum specified electric (E) field strength over the frequency range of 30 MHz to 1 GHz.
Class A equipment have protection limits at 10 m, and Class B equipment have protection limits at 3 m.
100 200 300 400 500 600 700 800 900 1000
Frequency (MHz)
Ptotal (dBm)
Class A: based on 10 m separation Class B: based on 3 m separation Class A: average limit Class B: average limit
Holloway et al., IEEE EMC Symposium
200 300 400 500 600 700 800 900 1000
Frequency (Hz)
E-field (dBV/ m) Reverb Chamber OATS
Relate total radiated power in reverberation chambers to measurements made on OATS with dipole correlation algorithms.
200 400 600 800 1000
Frequency (Hz)
E-field [dBV/ m] Reverb Chamber Anechoic Chamber
Total Radiated Power Comparison Max Field Comparison
The conventional methods uses normal incident plane-waves, i.e., Coaxial TEM fixtures.
E
i
E
t
⎟ ⎟ ⎠ ⎞ ⎜ ⎜ ⎝ ⎛ − =
i t
P P Log SE
10
10 However, these approaches determine SE for only a very limited set of incident wave conditions. In most applications, materials are exposed to complex EM environments where fields are incident on the material with various polarizations and angles of incidence. Therefore, a test methodology that better represents this type of environment would be beneficial.
Sample
⎟ ⎟ ⎠ ⎞ ⎜ ⎜ ⎝ ⎛ − =
ns in tx s in tx s in rQ ns in rQ s
ns
ns in r s in r
P P P P P P P P Log SE
, , , , , , , , , , , , , , , , 10 3
10
C.L. Holloway, D. Hill, J. Ladbury, G. Koepke, and R. Garzia, “Shielding effectiveness measurements of materials in nested reverberation chambers,” IEEE Trans. on Electromagnetic Compatibility, vol. 45, no. 2, pp. 350-356, May, 2003.
Sample
1 10
Frequency (GHz)
10 20 30 40 50 60 70 80
SE (dB)
aMaterial 1 Material 2 Material 3 Material 4 1 10
Frequency (GHz)
10 20 30 40 50 60 70 80 90
SE (dB)
aMaterial 2: with coating Material 2: with no coating
1 10
Frequency (GHz)
10 20 30 40 50 60 70 80 90
SE (dB)
aSE3: Chamber A SE3: Chamber B SE1: Chamber A SE1: Chamber B
intuition into loaded chamber responses to better help measurements
measured and modeled data, and use models to predict what we cant measure.
numerical code to explore multiple chamber
Descritize in to FDTD Grid Predict Stirred Fields Computationally to give us insight into chamber measurements in a loaded environment Take Real System Simulate
Large Lossy Body
Distributed Lossy Bodies Periodic Lossy Bodies
reverb chamber “small” enclosure
from the wall. This is because the tangential component of the E-field is zero are the wall. Thus, small monopole (or loop) probes attached to the wall can be used to determine the power in the center of a “small” enclosure.
statistics for the normal component of the E-field at the wall are the same for the field in the center of the chamber.
port 1 port 3 port 2 port 1 port 4 port 2 port 1 port 3 port 2 port 1 port 4 port 2
Mode-Stirred with a Horn Antenna: SE => S31 Mode-Stirred with a Monopole Antenna: SE => S41 Frequency Stirring with a Horn Antenna: SE => S31 Frequency Stirring with a Monopole Antenna: SE => S41
2 4 6 8 10 12 14 16 18 20 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000 Frequency (MHz) SE (dB)
mode_stirring_horn freq_stirring_horn mode_stirring_monopole freq_stirring_monopole
2 4 6 8 10 12 14 16 18 20 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000 Frequency (MHz) SE (dB)
mode_stirring_horn freq_stirring_horn mode_stirring_monopole freq_stirring_monopole
2 4 6 8 10 12 14 16 18 20 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000 Frequency (MHz) SE (dB)
mode_stirring_horn freq_stirring_horn mode_stirring_monopole freq_stirring_monopole
2 4 6 8 10 12 14 16 18 20 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000 Frequency (MHz) SE (dB)
mode_stirring_horn freq_stirring_horn mode_stirring_monopole freq_stirring_monopole
(c) narrow slot aperture (a) open aperture (b) half-filled aperture (d) generic aperture
5 10 15 20 25 30 35 40 45 50 3000 4000 5000 6000 7000 8000 9000 10000 11000 12000 Frequency (MHz) SE (dB)
Position 1, probe length=1.3 cm Position 2, probe length=1.3 cm Position 1, probe length=2.5 cm Position 2, probe length=2.5 cm
a=0.5 cm a=0.95 cm
5 10 15 20 25 30 2 2.5 3 3.5 4 Frequency (GHz) SE (dB) probe location 1 probe location 2 probe location 3 probe location 4
Dual-Ridged Horn used as receive antenna
Two paddles used
Antenna Under Test (AUT)
Results presented here are for relative total radiated power (RTRP) referenced to either a Horn or to a small Loop. For a Horn we have:
Horn AUT
where PAUT is the received power in the chamber when transmitting on the antenna under test (AUT), and PHorn is the received power in the chamber when transmitting on the horn. All antennas were connected to a 50 ohm cable, so results include both mismatch and efficiency (ohmic loss) effects.
If we assume the horn is the “best” antenna available, then these measurements will show how “well” an antenna is performing.
8 mm Loop for 612 MHz antenna 612 MHz antenna: loop with ten-layer spherical material
Comparison to Horn Comparison to Loops
500 550 600 650 700 750 800 850 900 950 1000
Frequency (MHz) Total Radiated Power Relative to Horn (dB) Ten-Layer Spherical Structure 8 mm Loop for 612 MHz Antenna 32mm Loop Antenna
5 10 15 20 500 550 600 650 700 750 800 850 900 950 1000
Frequency (MHz) Total Radiated Power Relative to Loops (dB) Comparison to 8 mm Loop Comparison to 32 mm Loop
New Magnetic Antenna Comparison to Horn Loop Antenna
5 200 250 300 350 400 Frequency (MHz) Total Radiated Power Relative to Horn (dB) Magnetic EZ-Antenna: Ground Plane-Center of Chamber Magnetic EZ-Antenna: No Ground Plane-Center of Chamber Magnetic EZ-Antenna: On Chamber Wall 3 cm Loop antenna
20 40 60 80 100 120 140 160 180 200 Location P (dBm) nor-xscan w/o material nor-xscan w metamaterial
Near-Field Antenna Tests
Extensive measurements have shown that when light of sight (LOS) path is present the radio multipath environment is well approximated by a Ricean channel, and when no LOS is present the channel is well approximated by a Rayleigh channel:
=
+ + + =
N n n n c n c LOS
t f f A t f A E
1
] ) ( 2 cos[ ) 2 cos( φ π π
The Amplitude of E is either Rayleigh or Ricean depending if a LOS path is present. Urban Environment Rural Environment
components scattered component direct k =
Paddle Transmitting Antenna metallic walls DUT
a a
We will show that by varying the characteristics of the reverberation chamber and/or the antenna configurations in the chamber, any desired Rician K-factor can be obtained.
Paddle DUT Transmitting Antenna metallic walls
2
2 3 r D Q V K λ =
It can be shown: see Holloway et al, IEEE Trans on Antenna and Propag., 2006.
Note:
pattern is used, it can be rotated with respect to the DUT, thereby changing the K-factor.
if r is small, K is large. This suggests that if the separation distance between the antenna and the DUT is varied, then the K-factor can also be changed to some desired value.
desired value. The Q of the chamber can easily be varied by simply loading the chamber with lossy materials. Also, if K becomes small, the distribution approaches Rayleigh. Thus, varying all these different quantities in a judicious manner can result in controllable K-factor over a reasonably large range.
Each set of curves represents a different distance of separation. The thick black curve running over each data set represents the K-factor obtained by using d determined in the anechoic chamber.
1.0E-04 1.0E-03 1.0E-02 1.0E-01 1.0E+00 1.0E+01 1.0E+02 1000 2000 3000 4000 5000 6000 7000 Frequency (MHz) K-factor
0.5 m 1 m separation 2 m separation
The thick black curve running over each data set represents the K-factor obtained by using d determined in the anechoic chamber.
1.0E-02 1.0E-01 1.0E+00 1.0E+01 1.0E+02 1.0E+03 1000 2000 3000 4000 5000 6000 7000 Frequency (MHz) K-factor
2 pcs absorber 6 pcs absorber 0 pcs absorber
The thick black curve running over each data set represents the K-factor obtained by using d determined in the anechoic chamber. Each data set was taken at 1 m separation and with 4 pieces of absorber in the chamber.
1.0E-03 1.0E-02 1.0E-01 1.0E+00 1.0E+01 1.0E+02 1000 2000 3000 4000 5000 6000 7000 Frequeency (MHz) K-factor
90 degrees 30 degrees 0 degrees
The thick black curve running over each data set represents the K-factor obtained by using d determined in the anechoic chamber. Each data set was taken at 1 m separation and with 4 pieces of absorber in the chamber.
1.0E-04 1.0E-03 1.0E-02 1.0E-01 1.0E+00 1.0E+01 1.0E+02 1.0E+03 1000 2000 3000 4000 5000 6000 7000 Frequency (MHz) K-factor
cross-polarized
45 degree polarization
co-polarized
2
) ( ) ( t h PDP = τ
Power Delay Profile:
where h(t) is the Fourier transform of S21 (ω)
∞ ∞
− =
2
dt t P dt t P t
) ( ) ( ) ( τ τ
∞ ∞
= dt t P dt t tP
( ) ( τ
One characteristic of the PDP that has been shown to be particularly important in wireless systems that use digital modulation is the rms delay spread of the PDP: where τo is the mean delay of the propagation channel, given by
2 2 2
1 1 1 2 2 2 ) ) (( ) ) ln( ( ) ( ) ( ln ) ln( K K Q
rms
+ − − + − + − + − − = α α α α α α ε α α α ω τ
Agilent 4438C Vector Signal Generator Agilent 89600 Vector Signal Analyzer External trigger Firewire connection to control VSA GPIB connection to control VSG Reverberation chamber
Demodulated 768ksps BPSK signal in I-Q diagram
facilities that have the capability of simulating any multipath environment for the testing of wireless communications devices.
functionality of the new emerging wireless devices in the future.
standards.