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© IMEC 2011 ESA PROJECT 1300008360 UWB RADIO FOR CABLE REPLACEMENT IN SATELLITES TECHNICAL NOTE 1.1 “HARDWARE DESCRIPTION, ENVIRONMENT AND TEST PLAN”

ESA project 1300008360 UWB radio for cable replacement in Satellites

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ESA project 1300008360 UWB radio for cable replacement in Satellites. Technical Note 1.1 “ Hardware description, environment and test plan ”. Introduction. Feasibility study for use of UWB radio for cable-replacements in intra-satellite communication. Project contains 3 activities: - PowerPoint PPT Presentation

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Page 1: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011

ESA PROJECT 1300008360UWB RADIO FOR CABLE REPLACEMENT IN SATELLITESTECHNICAL NOTE 1.1 “HARDWARE DESCRIPTION, ENVIRONMENT AND TEST PLAN”

Page 2: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011

INTRODUCTIONFeasibility study for use of UWB radio for cable-replacements in intra-satellite communication.

Project contains 3 activities:1. Hardware description, environment and test plan

Outcome: (TN1.1 = document)2. Measurement campaign

Outcome: (TN1.2a=Zip-file)3. Test report and analyses

Outcome: (TN1.2= > update of TN1.1) 2 versions: with and without confidential

informationThis presentation reports on TN1.2

2

Page 3: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011 3

OUTLINE OF THE DOCUMENT

1 Introduction ................................................................................. 1

2 IEEE802.15.4a UWB air interface........................................... 3

3 Top-level description of IMEC UWB transceivers..... ......... 11

4 Methodology................................................................................ 27

5 Venus express Mock-up description ......................................29

6 Channel Measurements and Modelling ................................. 33

7 Simulation framework and results ......................................... 67

8 Conclusions and recommendations....................................... 73

9 Bibliography................................................................................... 75

Page 4: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011 4

802.15.4A STANDARD

▸ 3 modes => mean Pulse repetition freq- 15.6 MHz- 3.9 MHz- 62.4 MHz

▸ 4 submodes => PHY bitrate- 27Mb/s- 6.8 Mb/s- 850 kb/s- 110 kb/s

▸ Off standard modes allow for other data rates as well- Use of ASIP/ASIC combination makes TX/RX

flexible! - Unique to IMEC technology

Page 5: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011 5

METHODOLOGY

Page 6: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011 6

ENVIRONMENT & MEASUREMENTS Parameters:▸ Satellite:

- Highly reflective environment- Significant reflection up to one microseconds

▸ BW:- 1-11 GHz (covers much communication

standards)- Time resolution => 100 picoseconds

▸ #FreqPoint > 1microsec/100picosec(=10k)▸ Nearest power of 2 => 16384 (DFT =>

FFT )▸ FreqStep = 610 kHz.

Result: H[f] => H(f)

Channel measurements showed the validity of these assumption

Page 7: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011 7

FREQ TO DELAY

Freq domain DFT Delay domain H[f,t] (=S21) <=> H[tau,t]Only valid if channel is constant

• True if doors are closed• Not guaranteed if doors are opened

Page 8: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011 8

MEASUREMENT REQUIREMENT

Measurement of H(f,t) takes approx 2 sec!Nothing may move more than 0.5cm over 2 seconds in relevant area!Relevant area = area relevant paths act. Do relevant paths exit & return from Mock-Up?

True if doors are closed False if doors are opened!

Page 9: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011 9

MEASUREMENT SETUP

=keyhole

Type amount

remark

Closed doors 36 6 intra cavity, 28 inter cavity, pathOpen doors 61 41*(5->6) + 20*(2->5)Antenna position

21 8*(5->5) + 5*(6->5) + 7*(2->5)

Page 10: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011

CHANNEL MEASUREMENT RESULTSPATH LOSS

3 4 5 6 7 8 9 10-70

-60

-50

-40

-30

-20

-10

0

Frequency [GHz]

Cha

nnel

Gai

n [d

B]

UWB [500 MHz]WLAN [20 MHz]Raw Data [610kHz]

1/f2

Channel gain as a function of carrier frequency with a sliding window.

Page 11: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011

0 0.5 1 1.5 2 2.5 3-60

-55

-50

-45

-40

-35

-30

-25

-20

#Keyholes

Cha

nnel

Los

s[dB

]

CHANNEL MEASUREMENT RESULTSPATH LOSS

Cavity 1 2 3 4 5 6

Path loss(dB)

-26 -25 -27 -25 -27 -27

Cavity Rx in 1

Rx in 2

Rx in 3

Rx in 4

Rx in 5

Rx in 6

Tx in 1 X -34 -41 -49 -50 -58

Tx in 2 -34 X -47 -42 -56 -53

Tx in 3 -41 -47 X -54 -41 -52

Tx in 4 -48 -41 -54 X -52 -42

Tx in 5 -50 -56 -41 -52 X -39

Tx in 6 -56 -52 -52 -42 -39 X

Channel gain as a function of the number of keyholes

Path losses (units in dB) for inter cavity measurements.

Large scale path loss

Page 12: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011

CHANNEL MEASUREMENT RESULTSIMPACT OF ANTENNA POSITION

3 4 5 6 7 8 9 10-100

-80

-60

-40

-20

0

Frequency [GHz]

Cha

nnel

Gai

n [d

B]

Measurement 1Measurement 2Measurement 3Measurement 4Measurement 5Measurement 6Measurement 7Measurement 8

Intra cavity measurements VNA channel 1 (Tx) and VNA channel 2 (Rx) in cavity 5 with 8 different antenna position configurations.

LOS, Close proximity

NLOS,Antennae at oppositeKey holes

Page 13: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011

CHANNEL MEASUREMENT RESULTSIMPACT OF OPEN DOORS

3 4 5 6 7 8 9 10-75

-70

-65

-60

-55

-50

000000000001000010000100001000010000100000000101001001001100010010100001100100101000001101100101101001101100101101111111

Effect of opening and closing of doors on the link-budget for inter cavity measurements VNA channel 1 (Tx) in cavity 2 and VNA channel 2 (Rx) in cavity 5 with many different door configuration. Doors 2 and 5 have the biggest impact.

• The opening of doors may lead to a channel gain loss up to 18 dB

Page 14: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011

CHANNEL MEASUREMENT RESULTSDELAY DOMAIN

0 200 400 600 800 1000 1200 1400 1600-160

-140

-120

-100

-80

-60

-40

time [ns]

S21

[dB

] Ban

dwid

th [1

0 G

Hz]

Real MeasurementSynthetic data

Real measured data for inter cavity measurement of cavity 1 to cavity 3, and synthetically generated data with the aid of two exponential functions and a noise floor describing the envelope.

Cavity 1 2 3 4 5 6

RMS delay

spread (ns)

40.7 37.5 34.6 16.0 35.8 34.9

Cavity Rx in 1 Rx in 2 Rx in 3 Rx in 4 Rx in 5 Rx in 6

Tx in 1 X 57.2 59.3 67.2 77.2 118.6

Tx in 2 56.3 X 73.2 46.6 109.5 80.0

Tx in 3 59.7 74.5 X 81.8 53.8 82.1

Tx in 4 69.0 47.5 82.6 X 77.9 44.6

Tx in 5 77.4 109.4 55.6 78.0 X 54.1

Tx in 6 110.6 75.8 81.4 44.1 52.3 X

RMS delay spread (units in ns) for inter cavity measurements.

Page 15: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011

CHANNEL MEASUREMENT RESULTSDELAY DOMAIN

0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.160

2

4

6

8

10

12

14

16

Amplitude [V]

Den

sity

Raw dataRicean fitRayleigh fit

Histogram of received signal voltage from 4 - 5 GHz and the estimated Ricean and Rayleigh distribution for both VNA channel 1 (Tx) and VNA channel 2 (Rx) in cavity 2.

Cavity 1 2 3 4 5 6

-17 -16 -14 -12 -18 -20

Cavity Rx in 1 Rx in 2 Rx in 3 Rx in 4 Rx in 5 Rx in 6

Tx in 1 X -23 -22 -22 -22 -24

Tx in 2 -22 X -24 -21 -24 -24

Tx in 3 -23 -22 X -23 -22 -24

Tx in 4 -22 -22 -22 X -22 -22

Tx in 5 -23 -24 -22 -23 X -23

Tx in 6 -24 -22 -24 -21 -23 X

Ricean factors (units in dB) for inter cavity measurements.

Small scale fading is Rayleigh distributed

Page 16: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011

CHANNEL MEASUREMENT RESULTSMINIMUM AND MAXIMUM PATH LOSSES

3 4 5 6 7 8 9 10-70

-60

-50

-40

-30

-20

-10

0

Frequency [GHz]

Cha

nnel

Gai

n [d

B]

UWB [500 MHz]WLAN [20 MHz]Raw Data [610kHz]

Intra cavity measurement in cavity 3 with 2σ confidence intervals over 1GHz windows. Solid line, UWB, striped line, WLAN, dotted line, Raw Data.

0 0.5 1 1.5 2 2.5 30

2

4

6

8

10

12

14

16

18

20

#Keyholes2

in

terv

al c

orre

spon

ding

to C

hann

el G

ain

[dB

]

UWB [500 MHz]WLAN [20 MHz]

The 2σ confidence intervals corresponding to the channel gain for the seven 1GHz windows for both intra and inter cavity measurements as a function of the number of 12 x 12 cm keyholes, i.e. hops.

• 2σ 5 dB mean power gain variation due to small scale fading. • Mean power mainly depends on cavity not on position

Page 17: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011 17

SIMULATION RESULTS

Flexible 802.15.4a simulation environment▸ Matlab

Complex-valued BB equiv. system model

non-coherent reception

Flexible PSDUsize

Added CRC16

Noise equal to measuredRXFE noise-figure

Iff CRC passes

Flexible Data rate/Modulation scheme

Page 18: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011 18

0 0.5 1 1.5 2 2.5 3 3.5 4

x 105

0

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1x 10

-3

Time

Ampl

itude

SHR preamble PHY header and Datapreamble

Preamble tracking and SFD Detection Payload decodingFine acquizition

SFD

SIMULATION RESULTS PER as measure for performance:▸ most honest but worse-case performance

criteria

Fine acquisition SFD

detection

PHY HDRdecoding

CRC check

Only successful reception if everything goes well.

Page 19: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011 19

PER WITH CLOSED DOORS

Many things can go wrong, but it does not;-) Reasons: ▸ Low average pathloss,

▸ highly reflective environment

▸ Keyholes are larger enough

▸ Hardly no small-scale fading▸ UWB is able to resolve

many multipath components

Page 20: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011 20

PER WITH OPEN DOORS Many things can go wrong, and here it does;-( With 1 hop everything is fine 3 hops is too much Reason: • Energy leaks into environment,

lowering RX powerBut:• ‘only’ 10 dB improvement needed• Link improvement are possible

• ↑TX power, ↓noise figure• Tailor BB processing• Network layer

Page 21: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011

CONCLUSION

The satellite’s radio channel is a high reflective/multipath-rich environment in which radio signal are able to propagate from one cavity to the next.

The large scale path loss of the channel for a frequency range of 3-10 GHz varies between -25dB (intra-cavity) to-58dB (cavity 1 to cavity 6) with closed doors.

The RMS delay spread varies between 40.7 ns (intra-cavity) and 118.6 ns (cavity 1 to cavity 6).

The small-scale-fading for narrowband systems is Rayleigh distributed even in LOS conditions. An example of such a narrowband system is 802.15.4. To obtain robust communication links, some form of diversity will be needed.

UWB systems experience a mean power gain variation of at most 5 dB due to small-scale-fading, due to its inherent frequency diversity.

The mean power gain of the channel depends mainly on the cavities of TX and RX, i.e. the exact position of the TX/RX within these cavities has little impact.

Page 22: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011 22

CONCLUSION

Opening of the satellite doors may lead to a decrease of the channel gain in the order of 15-18 dB for intra cavity channel and 10-13 dBs for inter cavity channels; depending on the contribution of the door as reflective object to the overall channel transfer function.

The most difficult channels are measured from cavity 1 to cavity 6 with open doors at high frequencies (6-10 GHz), where a mean power gain of -70 dB was recorded.

Imec’s current 802.15.4a-compliantUWB radio technology is able to provide for robust communication links at 600 kb/s netto data rate without packet loss:▸ from each cavity to every other cavity, if the doors are closed.▸ Very likely from each cavity to adjacent cavities with open doors.

Imec’s current 802.15.4a-compliant UWB radio technology is not able to provide for robust communication links from each cavity to every other cavity at 600 kb/s netto data rate without packet loss, if all doors are open and the cavity distance (hops) is larger than 1.

Page 23: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011

CHANNEL MEASUREMENT RESULTS

The satellite’s radio channel is a high reflective/multipath-rich environment in which radio signal are able to propagate from one cavity to the next.

The large scale path loss of the channel for a frequency range of 3-10 GHz varies between -25dB (intra-cavity) to-58dB (cavity 1 to cavity 6) with closed doors.

The RMS delay spread varies between 40.7 ns (intra-cavity) and 118.6 ns (cavity 1 to cavity 6).

The small-scale-fading for narrowband systems is Rayleigh distributed even in LOS conditions. An example of such a narrowband system is 802.15.4. To obtain robust communication links, some form of diversity will be needed.

UWB systems experience a mean power gain variation of at most 5 dB due to small-scale-fading, due to its inherent frequency diversity.

The mean power gain of the channel depends mainly on the cavities of TX and RX, i.e. the exact position of the TX/RX within these cavities has little impact.

Opening of the satellite doors may lead to a decrease of the channel gain in the order of 15-18 dB for intra cavity channel and 10-13 dBs for inter cavity channels; depending on the contribution of the door as reflective object to the overall channel transfer function.

Page 24: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011 24

RECOMMENDATIONS

EMC▸ Study ESA’s EMC requirement wrt FCC part

15 regulation for intentional radiators▸ EMC center Eindhoven could play a role!

Page 25: ESA project 1300008360 UWB radio for cable replacement in Satellites

© IMEC 2011 25

RECOMMENDATIONS

Centralized network topology▸ Only intra-cavity communication,▸ Inter cavity communication via wired bus

system▸ Increased system capacity▸ Beneficial if one of few data-sink can be

identified Ad-hoc network topology▸ Each sensor/tag may communicate to any

other sensor/tag▸ More complicated MAC (assuming no fixed

addressing)