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1 Japan Aerospace Exploration Agency Current Status of WINDS (Wideband Internetworking Engineering Test and Demonstration Satellite) Toshio Higuchi January, 2007 Japan Aerospace Exploration Agency (JAXA) APAN#23 Manila (January, 2007)

Current Status of WINDS (Wideband Internetworking Engineering Test and Demonstration Satellite)

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APAN#23 Manila (January, 2007). Current Status of WINDS (Wideband Internetworking Engineering Test and Demonstration Satellite) Toshio Higuchi January, 2007 Japan Aerospace Exploration Agency (JAXA). Objectives of WINDS program. - PowerPoint PPT Presentation

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1

Japan AerospaceExploration Agency

Current Status of WINDS

(Wideband Internetworking Engineering Test and Demonstration Satellite)

Toshio HiguchiJanuary, 2007

Japan Aerospace Exploration Agency (JAXA)

APAN#23 Manila (January, 2007)

2

Japan AerospaceExploration Agency

WINDS was established based upon “e-Japan program” of Japanese government in order to contribute a digital-divide free comfortable communication society by complementary utilization of ground based and satellite based communication network which has the following advantage: Wide Coverage, Broader Accessibility and Survivability against natural disaster

JAXA has been developing WINDS collaborating with National Institute of Information and Communication Technology (NICT).

JAXA: Total Network System Satellite System, Multi-Beam Antenna, Multi-Port Amplifier, Active Phased Array Antenna Ground System: Network Management Center, Regenerative Ground Terminals (USAT, HDR-VSAT) Satellite Tracking and Control SystemNICT: Onboard ATM Baseband Switching Router Bent-pipe Ground Terminals (LET, SDR-VSAT)

Objectives of WINDS program

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Japan AerospaceExploration Agency

1. Establishment of ultra-high-speed fixed satellite communications technologies High-Speed communication rate

Realization of ultra-high-data rate communication.• 155 Mbps for home use (small terminal with 0.45m diam.

class antenna ) • 1.2Gbps for business use (large station with 5m diam. class

antenna ) Wide coverage

Ultra-high-data rate communication in a wide area of Asia /Pacific region

Establishment of total system for high-speed satellite based communication network which realizes “flexible” user assignment.

2. Verification of ultra-high-data rate satellite based communications network Verification of management of the ultra-high-data rate satellite based communication network and promotion of experiments.

Objectives of WINDS program

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Japan AerospaceExploration Agency

WINDS            Conventional Satellite

Tx & Rx1.2Gbps

Tx & Rx

155Mbps

Rx155Mbp

s

Tx1.5Mbps

5m

Antenna Diameter of Ground Terminal

2.4m

0.75m

0.45m

1.2m

High speed data communication with small terminals by high EIRP with Ka-band multi-beam antenna and 8 parallel TWTA’s

Features of WINDS (1)

5

Japan AerospaceExploration Agency

Efficient Utilization of Satellite Resource by Onboard Switching Router.

A A

B B

C C

Onboard Switching Router

A

c

B

AB

CB

BB BBXPNDR

1 2 3 1 2 3AB

ビーム A

ビーム B

ビーム C

Deletion of empty cells

Prioritize packets in case of congestion

Features of WINDS (2)

WINDS             Conventional Satellite

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Japan AerospaceExploration Agency

Flexible power assignment by Ka-band high power Multi-Port Amplifier (MPA) and Multi-Beam Antenna (MBA)Effective power distribution depending upon requirements of compensation of rain attenuation and utilization demands

WINDS

Effective RF   power distribution

Using MPA

Clear sky area

Required power for clear sky

Conventional Satellite

Required power for rainy area

TX

po

wer

TX

po

wer

Rainy area Clear sky area

:fixed: adjustable

Rainy area

Features of WINDS (3)

7

Japan AerospaceExploration Agency

Launch Schedule End of FY2007 by H-IIA2024

Satellite Bus 2.4t, Zero-Momentum 3-Axis Stabilized

Orbital Location GEO@ 143°E (or 144.5, 146°E)

Generated Power 5,200 W

Mass 4,800 kg (launch), 2,400 (dry)

Frequency Band27.5 - 28.6 GHz (uplink)

17.7 - 18.8 GHz (downlink)

EIRP ≥ 67.3 dBW (FMBA), ≥ 55.0 dBW (APAA)

G/T ≥16.3 dB/K (FMBA), ≥ 7.1 dB/K (APAA)

On-Board SW

1.5/6/24/51/155 Mbps (uplink)

155 Mbps (downlink)

ATM Switching : 2.5 Gbps

Bent-Pipe RelayBW : 1.1 GHz

≤ 1.244 Gbps / transponder

WINDS

8

Japan AerospaceExploration Agency

Multi-beam antenna reflector for domestic coverage (2.4 mø)

Multi-beam antenna reflector for S.E. Asia coverage (2.4 mø)

On-board switching router

2.4-ton satellite busKa-band active phasedarray antenna (APAA)

Multi-beam antenna reflector for domestic coverage (2.4 mø)

Multi-beam antenna reflector for S.E. Asia coverage (2.4 mø)

On-board switching router

2.4-ton satellite busKa-band active phasedarray antenna (APAA)

External View of WINDS

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Japan AerospaceExploration Agency

Rx APAA

Tx APAA

650mm 540mm

470mm

290mm

Active Phased Array Antenna (APAA) can hop its beams to required points 2msec interval in order to cover the wide area.

APAA (Active Phased Array Antenna)

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Japan AerospaceExploration Agency

* Fixed beams cover Japan andseveral S. E. Asian areas

* Scanning beams by APAA coverother visible area

* Fixed beams cover Japan andseveral S. E. Asian areas

* Scanning beams by APAA coverother visible area

Antenna Beam Coverage

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Japan AerospaceExploration Agency

115 120 125 1305

10

15

20

25

Longitude [deg-E]

Latit

ude

[deg

-N]

-3-6

-10

-15

-20-25

-30

-30

-30

-30

-25

-30

-25

-30

-30

-25

WINDS A-MBA TX CO-POL (Manila beam)

-20

<Transmit Pattern><Transmit Pattern>

115 120 125 1305

10

15

20

25

Longitude [deg-E]

Latit

ude

[deg

-N]

-3-6

-10-15-20

-25

-30

-30

-30

-30

WINDS A-MBA RX CO-POL (Manila beam)

-25

-30

<Receive Pattern><Receive Pattern>

115 120 125 1305

10

15

20

25

Longitude [deg-E]

Latit

ude

[deg

-N]

-3-6

-10

-15

-20-25

-30

-30

-30

-30

-25

-30

-25

-30

-30

-25

WINDS A-MBA TX CO-POL (Manila beam)

-20

115 120 125 1305

10

15

20

25

Longitude [deg-E]

Latit

ude

[deg

-N]

-3-6

-10

-15

-20-25

-30

-30

-30

-30

-25

-30

-25

-30

-30

-25

WINDS A-MBA TX CO-POL (Manila beam)

-20

115 120 125 1305

10

15

20

25

115 120 125 1305

10

15

20

25

Longitude [deg-E]

Latit

ude

[deg

-N]

-3-6

-10

-15

-20-25

-30

-30

-30

-30

-25

-30

-25

-30

-30

-25

WINDS A-MBA TX CO-POL (Manila beam)

-20

<Transmit Pattern><Transmit Pattern>

115 120 125 1305

10

15

20

25

Longitude [deg-E]

Latit

ude

[deg

-N]

-3-6

-10-15-20

-25

-30

-30

-30

-30

WINDS A-MBA RX CO-POL (Manila beam)

-25

-30

115 120 125 1305

10

15

20

25

Longitude [deg-E]

Latit

ude

[deg

-N]

-3-6

-10-15-20

-25

-30

-30

-30

-30

WINDS A-MBA RX CO-POL (Manila beam)

-25

-30

115 120 125 1305

10

15

20

25

115 120 125 1305

10

15

20

25

Longitude [deg-E]

Latit

ude

[deg

-N]

-3-6

-10-15-20

-25

-30

-30

-30

-30

WINDS A-MBA RX CO-POL (Manila beam)

-25

-30

<Receive Pattern><Receive Pattern>

MBA Spot Beam Area (Manila Beam)

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Japan AerospaceExploration Agency

【 Network Management Center】

【 HDR-VSAT】

【 USAT】 【 Beaco

n Station】

155Mbps

155Mbps

【 LET 】※

~622Mbps~1.2Gbps

1.5M/6Mbps

155Mbps

1.5M/6Mbps

【 SDR-VSAT 】 ※

端末機 ODU/IDU

ワークステーション

ABS

SPOC

USBCMD/TLM

SOPS STAD SIMS

INIT

【 Tracking & Control

System】

【 WINDS

Satellite】

【 USAT】

端末機 ODU/IDU

Ka Band

※: by NICT

【 Ground System】

WINDS Network

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Japan AerospaceExploration Agency

Bent-pipe

  ~622Mbps × 21.2 Gbps

Bent-pipe~622Mbps

LET * >5mφ

SDR-VSAT * 2.4mφ

USAT 45cmφ

ABS *

DEM/ATMS/MOD

D/LWINDSU/L

HDR-VSAT 1.2mφ

USAT 45cmφ

1.5 - 6Mbps

155Mbps1.5~155Mbps

HDR-VSAT 1.2mφ155Mbps

※ : by  NICT

SDR-VSAT * 2.4mφ

LET * >5mφ

Ground Terminals vs Data Rate

14

Japan AerospaceExploration Agency

Antenna Diameter Area Beam Degenerative

(155Mbps) Non Degenerative

(622Mbps)

Domestic (MBA/ MPA) 45cm*2/ 1.2m 2.4m

Overseas (MBA/ MPA) 45cm*2/ 1.2m 2.4m

1beam working 2.4m 7m

Honolulu (APAA)

2 beam

working

5m 15m

1beam working 2.4m 5.5m

Sydney (APAA)

2 beam

working

3.8m 11m

WINDS Ground Station

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Japan AerospaceExploration Agency

D/C&

RX IFSWMTX

TX IFSWMTX

&U/C

ATM-basedBasebandSwitching

Subsystem(ABS)

BPF-WBPF-W

BPF-NBPF-N

Ka-bandMulti-port

Amp.

TXRFSW

TX ActivePhasedArray

Antenna

RX ActivePhasedArray

Antenna

RXRFSW&

LNA

Fixed MBA (Japan)Fixed MBA (S.E. Asia)

7

7

7

712

12

12

12

D/C U/C

SW Controller

Mission Configuration

16

Japan AerospaceExploration Agency

RXSWMTX

TXSWMTX

RXAPAA

TXAPAA

MBA Japan

MBAOversea

ATM(& DDEM, MOD)

ATM :ATM SwitchDDEM:Digital DemodulatorMOD :modulator

155Mbp155Mbpss

MBA JapanUSAT USAT/VSAT LATVSAT

1.5Mbps1.5MbpsKyusyu

Kinki

OkinawaMPA

Kanto

1.5Mbps(Max 14 link), 6Mbps, 24Mbps, 51Mbps : Regenerate ATM Link (51M x 3 for 155M)155Mbps : Regenerate ATM Link (51M x 3 for 155M)

Bent Pipe Link

MBA Oversea

ATM Switching Mode

17

Japan AerospaceExploration Agency

・・・

RXSWMTX

TXSWMTX

RXAPAA

TXAPAA

MBA Japan

MBAOversea

MPAMBA

Oversea

ATM(& DDEM, MOD)

ATM :ATM SwitchDDEM:Digital DemodulatorMOD :modulator

Kanto51Mbps x 51Mbps x 33

155Mbps155Mbps

Tohoku

Kanto

Kyusyu

Seoul

Jakarta

MBA Japan

USAT USAT/VSAT LATVSAT

1.5Mbps(Max 14 link), 6Mbps, 24Mbps, 51Mbps : Regenerate ATM Link (51M x 3 for 155M)155Mbps : Regenerate ATM Link (51M x 3 for 155M)

Bent Pipe Link

Manila

Multicast Mode

18

Japan AerospaceExploration Agency

RXSWMTX

TXSWMTX

RXAPAA

TXAPAA

MBA Japan

MBAOversea

ATM(& DDEM, MOD)

ATM :ATM SwitchDDEM:Digital DemodulatorMOD :modulator

155Mbp155Mbpss

MBA Japan

USAT USAT/VSAT LATVSAT

1.5Mbps1.5Mbps

MPA

155Mbps155Mbps

622Mbps622Mbps

1.5Mbps(Max 14 link), 6Mbps, 24Mbps, 51Mbps : Regenerate ATM Link (51M x 3 for 155M)155Mbps : Regenerate ATM Link (51M x 3 for 155M)

Bent Pipe Link

MBAOverse

a

Kanto

Kyusyu

Kinki

Manila

Kanto

Kyusyu

Kinki

Manila

Bent-pipe Mode

19

Japan AerospaceExploration Agency

• FY2001: Pre-project start• FY2003: Phase-B(Basic Design) • FY2004: Phase-C(Detailed Design) • FY2006: Phase-D(Assemly,Integuration&Tes

ting) Now:

Final Integration of the Flight Model is going on at the industries’ facility.A series of performance and environmental testing will start at JAXA’s Tsukuba Space Center next year. Launch: FY2007 by H-IIA launch vehicleFY: Japanese fiscal year (April-March)

Current Status

20

Japan AerospaceExploration Agency

USAT (45cmΦclass)

VSAT  (1.2mΦclass)

Okinawa beacon Terminal

Designed based on RR and ITU-R recommendations such as S.524-8 “Maximum permissible levels of off-axis e.i.r.p. density

S.726-1 “Maximum permissible level of spurious emissions from VSATs” S.729 “Control and monitoring function of VSATs”

SM.1541-1 “Unwanted emissions in the out-of-band domain”

Terrestrial Test System Development

21

Japan AerospaceExploration Agency

ODU

Outdoor

IDUPC

ODU-IDUPrivate Connection Cable

HUB

Indoor

USERUSER

Cable

1000Base-T

Interface of WINDS User terminals

22

Japan AerospaceExploration Agency

Back Bone PatchBack Bone Patch Access PatchAccess Patch

Digital Divide FreeDigital Divide Free MulticastMulticast

Back up for Back bone in case of contingency

ISPIX

In case of disaster:Image of stricken area Information to suffers

Broad Band Internet

E-learning among multi points

Contents distribution

High speed Internet service with small terminals

Temporary link for special events

Potential Application of WINDS

23

Japan AerospaceExploration Agency

(1) Pilot ExperimentsIn order to firmly facilitate the in-orbit experiments of WINS, pilotexperiments such as data storage and transmission experiments, e-learningexperiments etc. using a commercial communication satellite have been conducted aiming at, - verification of the experiment environment, procedure - promotion of WINDS utilization

(2) Basic ExperimentsJAXA and NICT are making plans of basic experiments for the engineering evaluation of WINDS network system and newly developed technology.

(3) Application Experiments Ministry of Internal Affairs and Communications will make an announcement of opportunity for WINDS application experiments.JAXA and NICT will support the ministry to facilitate the experiments by providing technical support and communication capability of WINDS.

Preparation for WINDS Experiments

24

Japan AerospaceExploration Agency

Asia Institute of Technology Asia Institute of Technology (Bangkok)(Bangkok)

WINDWINDSS

Tsukuba Tsukuba UniversityUniversity

Tokyo CampusTokyo Campus

Malaysia Multimedia University Malaysia Multimedia University (Malaysia)(Malaysia)

Screen Image

Materials

Image of Tokyo Campus(Lecturer)

Image of Tsukuba University(Images of class room, text, etc.) Chat system

e-Learning (Example of Mesh-type network)

25

Japan AerospaceExploration Agency

Full participation

Partial-Mesh Type Full-Mesh TypeStar typeBroadcast Type

BidirectionalOne way

WINDSCurrent System

Pilot Experiments

ControlRequestLink allocationData

ATM

RequestLink allocationData

e-Learning System

26

Japan AerospaceExploration Agency

Volcano

FloodForest fire

Understanding of the disaster

Accident at sea

Marine pollution

Typhoon

Earthquake

AlertStatus

Warning

Earth Observation

Disaster Monitoring by MODIS, ALOS

Disaster Authority

Grasp the statusDisaster Information Platform

SupportActivity

ExtractionSharing

Distribution of ALOS images through internet

Digital Asia ( Web GIS)

JAXA, ADRC

JAXA, AIT, Keio Univ.

Capacity building for Disaster management

JAXA 、 AIT 、 ADRCCapacity Building

Data

Existing Information

JAXA, MODIS Earth Stations

Affected people

Sentinel Asia Concept

27

Japan AerospaceExploration Agency

Container TypePortable

Type

WINDS Transportable Terminals

28

Japan AerospaceExploration Agency

Disaster-stricken Area

Portable WINDS Terminal(Disaster-stricken Area)

HeadquartersPortable Terminal

WINDS

Images from the site

Trace of cameraman

Gathering information by wearable camera

29

Japan AerospaceExploration Agency

Very large mobile communication

satellite

Residents in disaster areas

Information center

Providing services directly to personal terminals in disaster areas

Disaster monitoring

Data collectionInformation delivering to

personal terminals

Ultra high-speed communication

satellite

Earth observation

satellites

Positioning Satellites

Ground observation network

Concept of Disaster Management using Space Technology in Asia Pacific region

30

Japan AerospaceExploration Agency

Year 2005 2006 2007 2008 -

WINDS

ApplicationExperiment

Pilot Experiment

Practical UsePractical Use

BasicExperiment

Launch

RFP

Request for proposal concerning Application Experimentsusing WINDS to be announced by Ministry of Internal Affairs, and Communications (MIC)

Milestones for WINDS Experiments

31

Japan AerospaceExploration Agency

MIC Press Release: November 27, 2006

http://www.soumu.go.jp/joho tsusin/eng/Releases/Telecommunications/news061127 1.html

Conditions: Participants may use the transponder for the satellite free of cha

rge. Equipment for the ground station shall, in principle, be prepare

d by the participants. Participants may request to use (borrow) the ground station that the satellite development agencies plan to install. However, it may not be possible to agree to all requests due to limited availability.

All expenses incurred in connection with implementation of the experiments shall be borne by the participants.

Application form shall be submitted to MIC from February 1st to March 30th 2007.

Call for Proposals concerning to the WINDS applications experiments is underway.

Call for Proposals