doc.: ieee 802.22-06/0206r1 submission november 2006 ivan reedeslide 1 ranging and location for...
TRANSCRIPT
November 2006
Ivan ReedeSlide 1
doc.: IEEE 802.22-06/0206r1
Submission
Ranging and Location for 802.22 WRANsIEEE P802.22 Wireless RANs Date: 2006-11-15
Name Company Address Phone email
Authors:
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Ivan Reede Montreal,CA 514-620-86522 [email protected]
November 2006
Ivan ReedeSlide 2
doc.: IEEE 802.22-06/0206r1
Submission
Abstract
A means to range802.22 links from base stations to customer premise equipment
inter customer premise equipments distances
inter base stations distances
Means to apply obtained results to establish the geographic location of these devices
November 2006
Ivan ReedeSlide 3
doc.: IEEE 802.22-06/0206r1
Submission
Location methods
• There are two basic data acquisition methods– Direction Finding– Ranging
• Both can be used together to determine a location from another location
• Both can be used without the other to determine a location from a group of other locations
November 2006
Ivan ReedeSlide 4
doc.: IEEE 802.22-06/0206r1
Submission
Direction Finding
• Conventionally performed by CW systems– CW time difference of arrival at the sensors– Results obtained from difference in time of arrival– Time difference (phase) between arials is converted to bearing– Requires known stable wave front
Source
Arial 1
Arial 2
November 2006
Ivan ReedeSlide 5
doc.: IEEE 802.22-06/0206r1
Submission
Ranging
• Difficult for some legacy PHY layers• Difficult for some legacy MAC layers• Well suited for higher bandwidth (fast) (PHY)
November 2006
Ivan ReedeSlide 6
doc.: IEEE 802.22-06/0206r1
Submission
Ranging over OFDM
• Well suited for PHY layer• May be supported by MAC layer• Requires a conceptually simple addition
November 2006
Ivan ReedeSlide 7
doc.: IEEE 802.22-06/0206r1
Submission
• OFDM receivers inherently effect range bearing information collection in normal operations
• Such information is required for their operation• Such information has not yet been recognized in any public
documentation as range bearing• In a 6 MHz BW channel, 1 meter ranging resolution may be
achieved
By the following means...
OFDM System ExampleAssertion Overview
November 2006
Ivan ReedeSlide 8
doc.: IEEE 802.22-06/0206r1
Submission
OFDM System ExampleFounding Premises
• OFDM systems transmit using a plurality of carriers• These carriers are at slightly different frequencies at RF, but
are harmonically related at baseband• They are related by the fact that they are all transmitted
simultaneously in a package called an OFDM symbol
November 2006
Ivan ReedeSlide 9
doc.: IEEE 802.22-06/0206r1
Submission
• The source of the OFDM symbol is usually an IFFT device• The symbol output is generally composed of a sum of sine
and cosine waves• All of these sine and cosine waves
– Start at the beginning of each symbol– End at the end of each symbol– Sine waves begin and end with zero values– Cosine waves begin and end with full amplitude values at symbol edges
OFDM System ExampleModel Overview
November 2006
Ivan ReedeSlide 10
doc.: IEEE 802.22-06/0206r1
Submission
• The receiver is generally composed of an FFT device• This device acts as a multi-carrier QPSK or n-QAM
demodulator• Each carrier can be demodulated as QPSK, 16-QAM,
64-QAM or other• As such, the OFDM receiver extracts amplitude and
phase information from each carrier
OFDM System ExampleModel Overview
November 2006
Ivan ReedeSlide 11
doc.: IEEE 802.22-06/0206r1
Submission
• Current receiver designs use pilot carriers to align the constellation demodulation process
• Assume, by standardization– That a pilot carrier be emitted with a known phase
• The receiver, in aligning to this carrier, essentially effects a “phase lock” to this pilot
• It demodulates with a known phase resolution– ~±45° for QPSK, ~±7.5° for 64-QAM
OFDM System ExampleModel Overview
November 2006
Ivan ReedeSlide 12
doc.: IEEE 802.22-06/0206r1
Submission
To demodulate QPSKphase lock must be
much better than ±45°
OFDM System ExampleQPSK Constellation
November 2006
Ivan ReedeSlide 13
doc.: IEEE 802.22-06/0206r1
Submission
To demodulate 16-QAMphase lock must be
much better than ±19°
OFDM System Example16-QAM Constellation
November 2006
Ivan ReedeSlide 14
doc.: IEEE 802.22-06/0206r1
Submission
To demodulate 64-QAMphase lock must be
much better than ±7.5°
OFDM System Example64-QAM Constellation
November 2006
Ivan ReedeSlide 15
doc.: IEEE 802.22-06/0206r1
Submission
• Transmitters internally use at least one clock• The symbols they transmit are related to this clock• By transmitting an OFDM symbol, they inherently
broadcast their space-time reference frame, relative to their geolocation and their clock
OFDM System ExampleTransmitter Space-Time Reference Frame
November 2006
Ivan ReedeSlide 16
doc.: IEEE 802.22-06/0206r1
Submission
Tx
Symbols emanatingfrom the transmitter
Transmitted wave conveys the Tx's Space-time frame
OFDM System ExampleTransmitter Space-Time Reference Frame
November 2006
Ivan ReedeSlide 17
doc.: IEEE 802.22-06/0206r1
Submission
• If the receiver knew exactly at what time the symbol was sent by the transmitter, the receiver could determine the distance from the flight time
• The receiver lacks this knowledge• The receiver, however, can lock an internal time
base (i.e. a counter) to the received wave• The receiver can therefore create a relative
space-time frame from a received OFDM symbol
OFDM System ExampleReceiver Premises
November 2006
Ivan ReedeSlide 18
doc.: IEEE 802.22-06/0206r1
Submission
• Assume a transmitter emits an OFDM symbol that contains a pilot carrier whose frequency is 3 KHz
• The wavelength associated with this frequency is ~100 km.
• A 64-QAM receiver, can lock its time base to this pilot within ±7.5°
• This creates a receiver relative space-time frame– in a 0-100 km radius to a 2.08 km resolution
OFDM System ExampleFundamental Operating Principles
November 2006
Ivan ReedeSlide 19
doc.: IEEE 802.22-06/0206r1
Submission
1
1
vp
10 p
sam ples
0 0 . 063 0 . 13 0 . 19 0 . 25 0 . 31 0 . 38 0 . 44 0 . 5 0 . 56 0 . 63 0 . 69 0 . 75 0 . 81 0 . 88 0 . 94 11
0
1B a s e b a n d t im e d o m a in s ig n a l
D A C ou tp u t sam p le #
OFDM System ExampleTransmitted 3 Khz Wave Symbol
November 2006
Ivan ReedeSlide 20
doc.: IEEE 802.22-06/0206r1
Submission
A ±7.5° quantizationamounts to ±2.08 km
space-time uncertainty
OFDM System ExampleReceiver Space-Time Reference Frame
November 2006
Ivan ReedeSlide 21
doc.: IEEE 802.22-06/0206r1
Submission
A ±7.5° quantizationamounts to a
100 km range ±2.08 kmspace-time frame
uncertainty
Rx
Tx
OFDM System ExampleReceiver 3 Khz wave Space-Time Reference Frame
November 2006
Ivan ReedeSlide 22
doc.: IEEE 802.22-06/0206r1
Submission
A ±7.5° quantizationamounts to a
100 km range ±2.08 kmspace-time frame
uncertainty
Rx
Tx
Receiver 3KHz wave Space-time frame
OFDM System ExampleReceiver 3 Khz wave Space-Time Reference Frame Snapshot
November 2006
Ivan ReedeSlide 23
doc.: IEEE 802.22-06/0206r1
Submission
• Assume the transmitter emits an OFDM symbol that contains a pilot carrier whose frequency is 6 KHz
• The wavelength associated with this frequency is ~50 km.• A 64-QAM receiver, can lock its time base to this pilot
within ±7.5°• This creates a wrapped relative space-time frame
– in a 0-50 km radius to a 1.04 km resolution– in a 50-100 km radius to a 1.04 km resolution
OFDM System Example(cont.)
November 2006
Ivan ReedeSlide 24
doc.: IEEE 802.22-06/0206r1
Submission
Transmitted 6 KHz wave symbol
1
1
vp
10 p
sam ples
0 0 . 063 0 . 13 0 . 19 0 . 25 0 . 31 0 . 38 0 . 44 0 . 5 0 . 56 0 . 63 0 . 69 0 . 75 0 . 81 0 . 88 0 . 94 11
0
1B a s e b a n d t im e d o m a in s ig n a l
D A C ou tp u t sam p le #
OFDM System ExampleTransmitted 6 Khz Wave Symbol
November 2006
Ivan ReedeSlide 25
doc.: IEEE 802.22-06/0206r1
Submission
Rx
Tx
Receiver 3 and 6 Khz wave Space-time frame
OFDM System Example(cont.)
November 2006
Ivan ReedeSlide 26
doc.: IEEE 802.22-06/0206r1
Submission
A ±7.5° quantizationover 360° amounts to ±1.04 km resolutionover a 50 km range space-time frame
uncertainty
Rx
Tx
Receiver 6 Khz wave Space-time frame
The space-time framewraps twice through 360°
in a 100 km range
OFDM System Example(cont.)
November 2006
Ivan ReedeSlide 27
doc.: IEEE 802.22-06/0206r1
Submission
• Using both pilots, the OFDM 64-QAM receiver• May create a space-time frame
– With 1.04 km resolution– Within a 0-100 km radius
OFDM System Example(cont.)
November 2006
Ivan ReedeSlide 28
doc.: IEEE 802.22-06/0206r1
Submission
Transmitted 3 and 6 KHz waves symbol
1 .755
1 .755
vp
10 p
sam ples
0 0 .063 0 .13 0 .19 0 .25 0 .31 0 .38 0 .44 0 .5 0 .56 0 .63 0 .69 0 .75 0 .81 0 .88 0 .94 12
0
2B a s e b a n d t im e d o m a in s ig n a l
D A C ou tpu t sam p le #
OFDM System ExampleTransmitted 3 and 6 Khz Wave Symbol
November 2006
Ivan ReedeSlide 29
doc.: IEEE 802.22-06/0206r1
Submission
Rx
Tx
Receiver 3 and 6 Khz wave Space-time frame
Using both wavesyields an unwrapped
2 km resolution100 km range
space-time frame
OFDM System Example(cont.)
November 2006
Ivan ReedeSlide 30
doc.: IEEE 802.22-06/0206r1
Submission
• Assume the transmitter emits an OFDM symbol that contains a pilot carrier whose frequency is 12 KHz
• A 64-QAM receiver, can lock its time base to this pilot within ±7.5°
• Using these pilots, the OFDM 64-QAM receiver• May create a space-time frame
– With 0.52 km resolution– Within a 0-25 km radius– Within a 25-50 km radius– Within a 50-75 km radius– Within a 75-100 km radius
OFDM System Example(cont.)
November 2006
Ivan ReedeSlide 31
doc.: IEEE 802.22-06/0206r1
Submission
Transmitted 12 KHz wave symbol
1
1
vp
10 p
sam ples
0 0 . 063 0 . 13 0 . 19 0 . 25 0 . 31 0 . 38 0 . 44 0 . 5 0 . 56 0 . 63 0 . 69 0 . 75 0 . 81 0 . 88 0 . 94 11
0
1B a s e b a n d t im e d o m a in s ig n a l
D A C ou tp u t sam p le #
OFDM System ExampleTransmitted 12 Khz Wave Symbol
November 2006
Ivan ReedeSlide 32
doc.: IEEE 802.22-06/0206r1
Submission
Transmitted 3 and 6 and 12 KHz wave symbol
2 .227
2 .227
vp
10 p
sam ples
0 0 .063 0 .13 0 .19 0 .25 0 .31 0 .38 0 .44 0 .5 0 .56 0 .63 0 .69 0 .75 0 .81 0 .88 0 .94 14
2
0
2
4B a s e b a n d t im e d o m a in s ig n a l
D A C ou tpu t sam p le #
OFDM System ExampleTransmitted 3 and 6 and 12 Khz Wave Symbol
November 2006
Ivan ReedeSlide 33
doc.: IEEE 802.22-06/0206r1
Submission
Rx
Tx
Receiver 3 and 6 and 12 Khz wave Space-time frame
Using all 3 wavesyields an unwrapped0.52 km resolution
100 km rangespace-time frame
OFDM System Example(cont.)
November 2006
Ivan ReedeSlide 34
doc.: IEEE 802.22-06/0206r1
Submission
• With more pilot's, as follows
3000 100000 2083.33 5277.78 125006000 50000 1041.67 2638.89 6250
12000 25000 520.83 1319.44 312524000 12500 260.42 659.72 1562.548000 6250 130.21 329.86 781.2596000 3125 65.1 164.93 390.63192000 1562.5 32.55 82.47 195.31384000 781.25 16.28 41.23 97.66768000 390.63 8.14 20.62 48.83
1536000 195.31 4.07 10.31 24.413072000 97.66 2.03 5.15 12.215997000 50.03 1.04 2.64 6.25
Pilot Baseband Frequency (Hz)
Wavelength range (m)
'±7.5° rangeresolution (m)
'±19° rangeresolution (m)
'±45° rangeresolution (m)
OFDM System Example(cont.)
November 2006
Ivan ReedeSlide 35
doc.: IEEE 802.22-06/0206r1
Submission
Transmitted 12 pilot wave symbol
6 .411
6 .411
vp
10 p
sam ples
0 0 .063 0 .13 0 .19 0 .25 0 .31 0 .38 0 .44 0 .5 0 .56 0 .63 0 .69 0 .75 0 .81 0 .88 0 .94 110
5
0
5
10B a s e b a n d t im e d o m a in s ig n a l
D A C ou tpu t sam p le #
OFDM System ExampleTransmitted 12 Pilot Example Wave Symbol
November 2006
Ivan ReedeSlide 36
doc.: IEEE 802.22-06/0206r1
Submission
• Using multiple pilots, the OFDM 64-QAM receiver• May create a space-time frame
– With 1 m resolution– Within a 0-100 km radius
• It still does not know the transmitter to receiver distance
• It knows the space-time frame of the signal• It may lock its time base to that space-time frame
OFDM System Example(cont.)
November 2006
Ivan ReedeSlide 37
doc.: IEEE 802.22-06/0206r1
Submission
• The receiving station can respond to queries, in a manner synchronous to the center of this space-time frame.
• The initial transmitter, when it receives a response from the station, can also establish a similar space time frame
• The discrepancy between the transmitter's initial space-time frame and the responses space-time frame reveals the total flight time
• Taking into account that the receiver is able to receive 12 dB SNR signals, the phase lock of real receiver must be much better and the total travel time can be estimated to within ~±0.5m resolution
OFDM System Example(cont.)
November 2006
Ivan ReedeSlide 38
doc.: IEEE 802.22-06/0206r1
Submission
• Other stations, hearing query responses, may also perceive and measure space-time frame discrepancies.
• These discrepancies reveal flight times, within ~±0.5 m resolution
• A collectivity of stations can accumulate a wealth of space-time frame discrepancies
• Once collected and processed, this information reveals precise station location and channel characteristics
OFDM System Example(cont.)
November 2006
Ivan ReedeSlide 39
doc.: IEEE 802.22-06/0206r1
Submission
Ranging Based Location Methods
• Time Sum Of Arrival (TSOA)• Time Difference Of Arrival (TDOA)• Absolute Range
For more details seeJuly 2006 presentation
November 2006
Ivan ReedeSlide 40
doc.: IEEE 802.22-06/0206r1
Submission
Ranging Based Location MethodsGeolocation Ranging Web Possibilities
BS
CPE4
CPE3
CPE2CPE1
CPE5
Range web valuesmay reveal elevationinfo / coax-lead-line
length
Z
November 2006
Ivan ReedeSlide 41
doc.: IEEE 802.22-06/0206r1
Submission
OFDM Ranging SummaryCosts
• Requires minimal if any ranging abilities in CPEs• Requires at least three located waypoints, at the BS or CPE or
some other known terrain characteristics• Economical
– it better exploits existing OFDM hardware– the pilot tones are already there for constellation sync– no special ranging symbols, symbols may be data bearing– practically no overhead– less overhead than any other location method– no external costs (such as GPS system costs + intsalltaion)
• Does not require many added abilities out of the CPE
November 2006
Ivan ReedeSlide 42
doc.: IEEE 802.22-06/0206r1
Submission
OFDM Ranging SummaryBenefits
• Simple, the pilot tones are already there for constellation sync• Fast and precise results, from a single query-response
– Provides the required resolution– Provides enough resolution for 3d location, including feed lines– Provides support for fixed devices– Provides support for mobility detection and tracking
• Is amenable to processing gain means on range and precision• Is self supportive, does not require external technology assists• Provides the ranging information needed to geolocate devices in
a simple, economical, elegant, inband and transparent fashion
November 2006
Ivan ReedeSlide 43
doc.: IEEE 802.22-06/0206r1
Submission
Alternatives?
• Is there another way to achieve the same goals?• Can we adapt this to allow OFDMA support?
November 2006
Ivan ReedeSlide 44
doc.: IEEE 802.22-06/0206r1
Submission
Alternatives?
• Is there another way to achieve the same goals?• Can we adapt this to allow OFDMA support?
The answer is YES ... to both questions
November 2006
Ivan ReedeSlide 45
doc.: IEEE 802.22-06/0206r1
Submission
Guard and Cyclic Prefix Needs
• In order to avoid filtering problems and multipath effects– A prefix is usually added to the transmitted signal– This provides time for filters to stabilize and stop “ringing”
• At the beginning of each symbol– Allows the receiving PHY to have some slack in its sync
• This slack has the apparent negative effect– Of negating the timing precision of the system
• This can be compensated after the FFT process
November 2006
Ivan ReedeSlide 46
doc.: IEEE 802.22-06/0206r1
Submission
Guard and Cyclic Prefix Needs
v t( )
0
N 1
k
I k ei
2 k t
T
=
ii
0 t T
v t( )
0
N 1
k
I k ei
2 k t
T
=
ii
Tg
t T
November 2006
Ivan ReedeSlide 47
doc.: IEEE 802.22-06/0206r1
Submission
Guard and Cyclic Prefix Needs
2
1 .125
vp
10 p
sam ples
0 0 .063 0 .13 0 .19 0 .25 0 .31 0 .38 0 .44 0 .5 0 .56 0 .63 0 .69 0 .75 0 .81 0 .88 0 .94 12
1
0
1
2B a s e b a n d t im e d o m a in s ig n a l
D A C ou tpu t sam p le #
Starting discontinuity Tail end always aligns with the starting discontinuity
November 2006
Ivan ReedeSlide 48
doc.: IEEE 802.22-06/0206r1
Submission
Guard and Cyclic Prefix Needs
2
1 .125
vp
10 p
sam ples
0 0 .063 0 .13 0 .19 0 .25 0 .31 0 .38 0 .44 0 .5 0 .56 0 .63 0 .69 0 .75 0 .81 0 .88 0 .94 12
1
0
1
2B a s e b a n d t im e d o m a in s ig n a l
D A C ou tpu t sam p le #
Starting discontinuity has been masked by copyingtail end and inserting itas a cyclic prefix
November 2006
Ivan ReedeSlide 49
doc.: IEEE 802.22-06/0206r1
Submission
Guard and Cyclic Prefix Needs
2
1 .125
vp
10 p
sam ples
0 0 .063 0 .13 0 .19 0 .25 0 .31 0 .38 0 .44 0 .5 0 .56 0 .63 0 .69 0 .75 0 .81 0 .88 0 .94 12
1
0
1
2B a s e b a n d t im e d o m a in s ig n a l
D A C ou tpu t sam p le #
Initial filter ringing and inter-symbol interference has the time to decay before acquisition begins
November 2006
Ivan ReedeSlide 50
doc.: IEEE 802.22-06/0206r1
Submission
Guard and Cyclic Prefix Needs
2
1 .125
vp
10 p
sam ples
0 0 .063 0 .13 0 .19 0 .25 0 .31 0 .38 0 .44 0 .5 0 .56 0 .63 0 .69 0 .75 0 .81 0 .88 0 .94 12
1
0
1
2B a s e b a n d t im e d o m a in s ig n a l
D A C ou tpu t sam p le #Signal acquisition interval does not have to be precisely aligned to get a valid orthogonal signal set
November 2006
Ivan ReedeSlide 51
doc.: IEEE 802.22-06/0206r1
Submission
Handling Guard and Cyclic Prefix
• Any time domain offset is mapped in the frequency domain• By a phase offset set in the recovered pilot carriers
– Phase offset values are proportional to pilot carrier frequency• The MAC may then compute the corresponding time offset
– Feed it back to the PHY for direct time stamp correction– Transmit correction data to the BS and other CPEs
• The BS receiving correction may compensate time offsets• Relaying CPEs have the option of
– Compensating– Relaying a compounded value back to the BS
November 2006
Ivan ReedeSlide 52
doc.: IEEE 802.22-06/0206r1
Submission
Guard and Cyclic Prefix Needs
2
1 .125
vp
10 p
sam ples
0 0 .063 0 .13 0 .19 0 .25 0 .31 0 .38 0 .44 0 .5 0 .56 0 .63 0 .69 0 .75 0 .81 0 .88 0 .94 12
1
0
1
2B a s e b a n d t im e d o m a in s ig n a l
D A C ou tpu t sam p le #
In the following examplewe will assume acquisitionstarted 12.5uSec before thereal symbol start
November 2006
Ivan ReedeSlide 53
doc.: IEEE 802.22-06/0206r1
Submission
Computing the PHY “slop”
• The PHY in its reception process– Acquires samples of the incoming signal– May establish a “sloppy” sync to symbol boundaries– Pass this “sloppy symbol” to the FFT– Which takes the acquires samples and decodes them– Into an array of vectors in an array of constellations
November 2006
Ivan ReedeSlide 54
doc.: IEEE 802.22-06/0206r1
Submission
Handling Guard and Cyclic Prefix
Rotation is mappedto acquisition delay
3 KHz pilot tone
-15° ± 7.5°± 6.25 uSec± 2km
• The MAC can then acquire a first-order fix– By examination of the lowest frequency carrier– Normalize the array of vectors to this lowest frequency vector– This normalization yields a first order “slop” correction term
• The MAC can then predict the next tone angle
November 2006
Ivan ReedeSlide 55
doc.: IEEE 802.22-06/0206r1
Submission
Handling Guard and Cyclic Prefix
Higher frequency pilot carrier is rotated more thanlower frequencypilot carrier
6 KHz pilot tone
• The MAC can then– Refine its error estimate by examining the next carrier– This normalization yields a higher order correction term
• Prediction in this example was 30° ± 15° (± 2 km)– This step reduces the ± 2 km down to ± 1 km
• The MAC can then predict the next tone angle
-30° ± 7.5°± 3.125uSec± 1 km
November 2006
Ivan ReedeSlide 56
doc.: IEEE 802.22-06/0206r1
Submission
Handling Guard and Cyclic Prefix
12 KHz pilot tone
• Repeat the process with ever increasing frequency carriers– Until the desired range resolution is obtained
-60° ± 7.5°± 1.56 uSec± 500 m
November 2006
Ivan ReedeSlide 57
doc.: IEEE 802.22-06/0206r1
Submission
Handling Guard and Cyclic Prefix
24 KHz pilot tone
• Repeat the process with ever increasing frequency carriers– Until the desired range resolution is obtained
-120° ± 7.5°± 0.78 uSec± 250 m
November 2006
Ivan ReedeSlide 58
doc.: IEEE 802.22-06/0206r1
Submission
Handling Guard and Cyclic Prefix
192 KHz pilot tone
384 KHz pilot tone
-240° ± 7.5°± 0.39 uSec± 125 m
-480° ± 7.5°± 0.20 uSec± 62.5 m
November 2006
Ivan ReedeSlide 59
doc.: IEEE 802.22-06/0206r1
Submission
Handling Guard and Cyclic Prefix
768 KHz pilot tone
1536 KHz pilot tone
-960° ± 7.5°± 0.10 uSec± 31.25 m
-1920° ± 7.5°± 0.05 uSec± 15.6 m
November 2006
Ivan ReedeSlide 60
doc.: IEEE 802.22-06/0206r1
Submission
Handling Guard and Cyclic Prefix
768 KHz pilot tone
1536 KHz pilot tone
-3840° ± 7.5°± 0.025 uSec± 8 m
-7860° ± 7.5°± 0.0125 uSec± 4 m
November 2006
Ivan ReedeSlide 61
doc.: IEEE 802.22-06/0206r1
Submission
Handling Guard and Cyclic Prefix
3072 KHz pilot tone
5997 KHz pilot tone
-15360° ± 7.5°± 0.0063 uSec± 2 m
-29985° ± 7.5°± 0.003 uSec± 1 m
November 2006
Ivan ReedeSlide 62
doc.: IEEE 802.22-06/0206r1
Submission
Compensating the PHY “slop”
• Once the desired resolution is reached• Store the normalization offset• Upon request from the BS, the CPE can transmit
– The normalization “space-time frame” time offset– The OFDMA “space-time” time offset to compensate flight time
November 2006
Ivan ReedeSlide 63
doc.: IEEE 802.22-06/0206r1
Submission
Guard and Cyclic Prefix Needs
2
1 .125
vp
10 p
sam ples
0 0 .063 0 .13 0 .19 0 .25 0 .31 0 .38 0 .44 0 .5 0 .56 0 .63 0 .69 0 .75 0 .81 0 .88 0 .94 12
1
0
1
2B a s e b a n d t im e d o m a in s ig n a l
D A C ou tpu t sam p le #
MAC knows that PHY acquisition frame is off set by 12.500 ±0.003 uSec
November 2006
Ivan ReedeSlide 64
doc.: IEEE 802.22-06/0206r1
Submission
Accommodating Guard
• This process allows for both– Real-life OFDM Receiver PHY sync limitations– OFDMA operation
• Where many CPEs – Share carrier resources in a given channel– Transmit in such a way to have all CPE space-time frames
• Arrive simultaneously at the BS• With space-time frame timing offset data
• This process allows the BS confirm its range estimates– By requesting a CPE additional pilots in OFDMA mode
November 2006
Ivan ReedeSlide 65
doc.: IEEE 802.22-06/0206r1
Submission
Pilot Tone Selection
• It is very important to understand– The the choice of a dozen pilots in these examples
• Is arbitrary, for example purposes only• Can dynamically be reduced or increased to
– Accommodate channel characteristics– Provide more statistical data– Allow for processing gain and artifact reduction
• In good 64-QAM, line of sight channels, 4 pilots are sufficient• In bad channels, many more pilots may be desired
– To compensate noise– To counteract and discard deviant pilot readings
November 2006
Ivan ReedeSlide 66
doc.: IEEE 802.22-06/0206r1
Submission
Resolution is NOT Precision
• It is very important to understand– That although this system has 2m/100km resolution capability– In practice, absolute precision is always lower than resolution
• Channel artifacts limit precision in radio-location systems– Mutipath (reflections, scatter, refraction-index variance)– Doppler, fading, weather-related media properties, etc...– They apply in various degrees to ALL radio-location systems– ALL radio-location systems are subject to similar limitations
• The goal is to meet 802.22 network geolocation precision needs– 100m for 67% of cases, 300m for 95% of cases; in a 100km range– 1km positional stability (CPE motion-cutoff threshold)
November 2006
Ivan ReedeSlide 67
doc.: IEEE 802.22-06/0206r1
Submission
Providing for OFDMA Flexibility
• It is proposed that a MAC to MAC primitive be created• To allow a CPE MAC to inform any receiving MACs• About the time offset value included in an emanated time frame
– At least 17 bits are needed for 1m resolution at 100km• To allow CPEs to transmit offset space-time frames to
• Allow transmission at an opportunistic time for OFDMA• Accommodate CPE Rx sync limitations• Future enhancements
• So the receiving MAC may – take into account said space-time frame “time” offset
November 2006
Ivan ReedeSlide 68
doc.: IEEE 802.22-06/0206r1
Submission
Providing OFDMA Hooks
• It is proposed that a MAC protocol primitive– Allows for inclusion or suppression from a CPE's spectrum
• Of the ranging pilots• To allow for OFDMA operation
– Without superposition of standard ranging pilots• From a universe of CPEs
• Optionally, if it is easy and simple– Allow the BS to specify alternate CPE to BS ranging carriers
• To allow coherent, simultaneous ranging of many CPEs• Validate and verify range estimates
November 2006
Ivan ReedeSlide 69
doc.: IEEE 802.22-06/0206r1
Submission
MAC Assisted Ranging SummaryBenefits
• Fast and precise results, from a single query-response– Provides the required resolution without high-speed clocks– Provides for OFDMA operation with real-life add-ons
• Is amenable to processing gain– Statistical processing can, over multiple samples
• Quantify, via standard deviation analysis– Noise and multi-path instability
• Reduce, by algorithms performing averaging processes– Noise (i.e. Effectively reducing BW)– Analyze unstable multi-path artifacts (wobble, Doppler...)
– Perform and correct for CPE clock drift and offset
November 2006
Ivan ReedeSlide 70
doc.: IEEE 802.22-06/0206r1
Submission
MAC Assisted Ranging SummaryBenefits
• Opens an opportunity to understand and and differentiate– Artifacts that are CPE specific– Artifacts that affect many CPEs in a region– Artifacts that affect all CPEs connected to a BS
• Analyze and understand how these artifacts affect the channel• Reduce, by futur algorithmic analysis
– Errors caused by these artifacts– Take corrective action
This may only be possible for in-band radio-location means
November 2006
Ivan ReedeSlide 71
doc.: IEEE 802.22-06/0206r1
Submission
MAC Assisted Ranging SummaryBenefits
• Simple, the pilot tones are already there for constellation sync– Pilot tone set may be flexible
• Accommodates fading• Avoids worst-case fading pilot carrier frequencies• Allows the BS to explore the channel characteristics
• Is self supportive, does not require external technology assists– Hardware time stamp is already needed for OFDMA– Extreme temporal precision is achieved by processing gain
• Provides the ranging information needed to geolocate devices in a simple, economical, elegant, inband and transparent fashion
November 2006
Ivan ReedeSlide 72
doc.: IEEE 802.22-06/0206r1
Submission
Topic for Jan 2007“Fractal Propagation” Location
BS