HIGH-SPEED DOWNLINK COMMUNICATIONS WITH ......Satellite points earth station D H α feed points...

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HIGH-SPEED DOWNLINK COMMUNICATIONS WITH HUNDREDS Mbps FROM 50kg CLASS SMALL SATELLITES Hirobumi Saito Japan Aerospace Exploration Agency (JAXA), Institute of Space and Astronautical Science (ISAS) Naohiko Iwakiri , Atsushi Tomiki, Takahide Mizuno, Hiromi Watanabe, Tomoya Fukami, Osamu Shigeta, Hitoshi Nunomura, Yasuaki Kanda , Kaname Kojima, Takahiro Shinke, and Toshiki Kumazawa

Transcript of HIGH-SPEED DOWNLINK COMMUNICATIONS WITH ......Satellite points earth station D H α feed points...

Page 1: HIGH-SPEED DOWNLINK COMMUNICATIONS WITH ......Satellite points earth station D H α feed points Onboard Small Antenna Body-Fixed Iso-flux Antenna 5dBi max, 150g qaudrafilar helix 150g,

HIGH-SPEED DOWNLINK COMMUNICATIONS WITH HUNDREDS

Mbps FROM 50kg CLASS SMALL SATELLITES

Hirobumi Saito

Japan Aerospace Exploration Agency (JAXA), Institute of Space and Astronautical Science (ISAS)

Naohiko Iwakiri , Atsushi Tomiki, Takahide Mizuno, Hiromi Watanabe, Tomoya Fukami, Osamu Shigeta, Hitoshi Nunomura, Yasuaki Kanda ,

Kaname Kojima, Takahiro Shinke, and Toshiki Kumazawa

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Contents

1. Purpose : 320Mbps down link for small sat

2. Onboard segment: high effiency transmitter.

small antenna

3. Ground segment : 3.8m S/X band antenna

powerful receiver

4. Total simulation : SPW software + link calculation

5. On-orbit demonstration : 2014 with 50kg sat.

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Limits of Small Satellites for Earth Observations

• Mass Limit(<100kg), Power Limit (<100W)

ー Telescope Resolution (5m vs. 0.5m)

ー Down link Speed (10Mbps vs. 800Mbps)

・ What is the Bottleneck of Down Link Speed ?

- Power !

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Down link bit rate VS. satellite mass for low earth orbit.

ERSEnvisat1

TRMM

Radarsat1

Spot

IRS-1A,1B,1CAS1000

JERS1

ADEOS

ALOS

MOS 1AMOS 1B

EOS-PM1

Landsat

Terra

Ikonos2

Orbview2

Orbview4Orbview3

TOMS-EP

GeoEye-1

TerraSAR-X

AlSat

TopSat

PRISM

UK-DMC1

UK-DMC2

WorldView1

QuickBird2

EROS-B

Kompsat2

EROS-A

Formosat2

RazakSat-1

EarlyBird

Lewis

MicroLabSat

Cute-I

Cute-1.7

1.0E+03

1.0E+06

1.0E+09

1.0E+12

1 10 100 1000 10000

観測衛星のデータ伝送速度(

bps)

衛星質量(kg)

Do

wn

Lin

k B

it R

ate(

bp

s)

Hodoyoshi #4

(2014)

Satellite Mass (kg)

1T

1G

1M

1K

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High Speed Down Link for Small Sat

• Purpose of This Research:

High-speed Down Link System

with Low Power Consumption

―Goal

50kg Sat @600km orbit

DC power <20W, 320Mbps

Small Ground Antenna < 4m

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System block diagram of high-data-rate downlink.

CCSDS-Formated

Data

Low Pass Filter

RF Amp

I-Q Mod

GaN Amplifier high efficiency & small distortion

Simple memoryless look – up - table

Simple digital circuit X2.5 oversampling with analog filter

Ground Demodulator

Turbo equalizer, Turbo decoder

Small S/X dual band parabolic antenna

Data

Small X band antenna

I/Q Map

Satellite Transmitter

UP- Con

I

Q

Cal A Cal B FPGA Cal C

Pre-Distortion

Pulse Shaping Filter

D/A

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Performance of High - Data - Rate Down Link

Instruments Mass

(g)

 Power

(W)

Remarks

On-board

Transmitter 1330 18 16QAM, 348Mbps

GaN Power Amp.

Antenna

MGA 69 0 14.6 dBi

Iso-flux 150 0 5dBi(60°),-2dBi(0°)

Antenna

Demodulator

Ground Station

3.8m Dia. S/X Cassegrain

48dBi(X), 36dBi(S)

100Msps, (348-144Mbps), 16QAM, QPSK

SCCC Turbo Equalizer CCSDS 131.0.

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High-Speed 16QAM Down Link with Nonlinear Amplifier

High efficiency RF amplifier may degrade bit error rate

Q

I

102

18

Input IQ Constellation

Nonlinear Amplifier Output I-Q Constellation

1 sumbol transmits 4 bits AM & PM

Distortion

位相回転

Inter Symbol Interference

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Digital Pre-distortion compensates Nonlinearity

PM compensation

Pre-Distortion Nonlinear RF amplifier

Pulse

Shape

Filter

RF out

Small

Distortion

Mod AM compensation

AM - PM

AM - PM

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X Band Power Amplifiers

Newly Developed 2W GaN HEMT AB Class

3cm

Amplifier GaAs AB GaN AB GaN F

Maximum Power 38dBm 37dBm 36dBm

Maximum Gain 10dB 11dB 12dB

Maximum PAE 37% 46% 60%

PAE at 3dB OBO 23% 36% 38%

Maximum Phase Shift 10° -2° -34°

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AM/AM AM/PM IQ Constellation

Without Pre-distortion

GaAs (AB)

GaN (AB)

GaN (F)

Ph

ase

Sh

ift

[deg

ree]

Ou

tpu

t [d

Bm

]

Input [dBm]

Input [dBm]

Ph

ase

Sh

ift

[deg

ree]

Ou

tpu

t [d

Bm

]

Input [dBm]

Input [dBm]

Ph

ase

Sh

ift

[deg

ree]

Ou

tpu

t [d

Bm

]

Input [dBm] Input [dBm]

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GaAs (A)

AM/AM AM/PM IQ Constellation

Without Pre-distortion

With Pre-distortion

GaN (AB)

GaN (F)

Ph

ase

Sh

ift

[deg

ree]

Input [dBm]

Ph

ase

Sh

ift

[deg

ree]

Ou

tpu

t [d

Bm

]

Input [dBm]

Ou

tpu

t [d

Bm

]

Input [dBm] Input [dBm]

Ou

tpu

t [d

Bm

]

Input [dBm]

Pre-distortion

Input [dBm]

Ph

ase

Sh

ift

[deg

ree]

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EM of 348 Mbps Transmitter

1330g, 18WDC, 16QAM measured I-Q map w/o pre-distortion

Pre-distortion will be installed soon

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Onboard Small Antenna Body-Fixed Medium Gain Antenna

14 dBi, 68g

Feed point

Active element

Passive element

Satellite

3.8m Ground Station

14 dBi, 68g, 7x7cm

For 320Mbps high bit rate mode,

Satellite points earth station

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D

H

α

feed

points

Onboard Small Antenna Body-Fixed Iso-flux Antenna

5dBi max, 150g

qaudrafilar helix 150g, D=10mm, H=20m

For Earth-Pointing Satellite, Antenna pattern compensates

range variation

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Ground Antenna 3.8m Ground Antenna for S / X Band

S band : Telemetry & Command X band : Mission Data Down Link (320Mbps)

Ring-Focus Cassegrain

(3m S band)

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Block diagram of high-data-rate downlink

and ground receiver

Receiver

ComplexNCO

Phasedetector

Signalsearcher

Signalresampler

Loopfilter

Timingdetector

↓2

Loopfilter

Frequency tracking loop (FTL)

Timing tracking loop (TTL)

nr SCCCturbo equalizer

ˆia

Matchedfilter

Packet generator

Poweramplifier

SRRCfilter

AWGNFreq.shift

iaRF

BPF

Phasenoise

Transmitter

Pre-distortion

Developing 400Mbps 16QAM ground receiver

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Block diagram of high-data-rate downlink

and ground receiver

Receiver

ComplexNCO

Phasedetector

Signalsearcher

Signalresampler

Loopfilter

Timingdetector

↓2

Loopfilter

Frequency tracking loop (FTL)

Timing tracking loop (TTL)

nr SCCCturbo equalizer

ˆia

Matchedfilter

Packet generator

Poweramplifier

SRRCfilter

AWGNFreq.shift

iaRF

BPF

Phasenoise

Transmitter

Pre-distortion

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Simulation Required Eb/N0 for BER = 10-6

16QAM

QPSK

Coding Rate

E b/N

o(d

B)

without pre-distortion

linear channel

with pre-distortion

GaN AB Amplifier

CCSDS 131.0 SCCC

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Link margin of high-data-rate down (2W GaN HEMT of AB class with pre-distortion)

1 2 3 4 5 6 13 14 15 16 ACM

320 Mbps 14 dBi MGA +3.8m Groun Ant EL= 30°

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Project Schedule

Onboard Tranmitter ’12 Aug-Oct T EM test ‘13 Feb-April FM test ‘13 May FM system test Ground Antenna ’13 March Complete Ground Receiver ’12 Dec. First test ‘13 March Complete ? Hodoyoshi -#4 (60kg) Launch ‘13 Dec. by Dnepr ’14 Demonstration 320Mbps 16QAM test on orbit

Now !

Goal !

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Conclusions

1. Developing 320Mbps 16QAM down link for 50kg satellite.

2. Power-efficient transmitter

(GaN HEMT amp with predistortion)

small antenna (MGA, isoflux)

3. Small ground antenna,

powerful receiver (turbo equalizer & decoding)

4. On-board demonstration in 2014 with 50kg sat.