aac presentation 11 nov snsb public pdf satellitprojekts låg...stefan hanna (deputy mayor uppsala,...
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![Page 1: AAC presentation 11 nov SNSB public pdf satellitprojekts låg...Stefan Hanna (Deputy Mayor Uppsala, f.m. Ericsson, IBM, Industrimatematik) Olof Stjernberg ... OBC / RTU lite 500 µRTU](https://reader034.vdocuments.mx/reader034/viewer/2022051722/5aa983727f8b9a9a188d0677/html5/thumbnails/1.jpg)
Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 1
ÅAC Microtec
– Nano/microsatellites and subsystems –
11 November 2011. SNSB, Solna
ÅAC Microtec ABDag Hammarskjölds väg 54B,
Uppsala Science ParkSE-751 83 Uppsala, SwedenE: [email protected]
P: +46 18 560130
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 2
About ÅAC Microtec AB…
� Formerly named Ångström Aerospace Corporation
� Two business units� Space and Defense
� Miniaturized and Robust Industrial Electronics
� Academic spin-off company from Uppsala University, The Ångström Laboratory
� Privately owned
� Semiconductor production class (100) clean rooms
� Turn over ~ €3.5M Euro
� CEO, Mats Magnell (f.m. Scania, Mydata, ABB)
� V.P. Space & Defense, Dr. Fredrik Bruhn
� Corporate Board
� ChairmanSven Löfqvist (f.m. CEO Micronic Laser Systems)
� Stefan Hanna (Deputy Mayor Uppsala, f.m. Ericsson, IBM, Industrimatematik)
� Olof Stjernberg (board member C2SAT, f.m. CEO Wasakredit)
� Johan Bäcke, RP Ventures
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 3
ÅAC world wide locations
AAC Microtec North America Inc.NASA Ames Research CenterBuilding 19 Room 2024Moffett Field, CA 94035, USA
ÅAC Microtec ABDag Hammarskjölds väg 54 B751 83 Uppsala, Sweden
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 4
Advanced Packaging Si-interposer Technology Featuring XiVIA™
� Ruggedized for space temperature range.� Licensed to Silex Microsystems and used in hermetic Met-Cap™ packaging for
medtech.� Under qualification with ESA as ”harmonized” packaging technology for 3D
integrated electronics
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 5
Example miniaturized avionics and power subsystems
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 6
Lowering cost in space business
US Air Force Research Laboratory,PnPSat-1 AIT
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 7
Swedish-US Defense MOU
Project Agreement (PA)
Swedish Defence Materel Administration (FMV)
PM: Jerker Fredén
Senior Adv.: Cmd. (ret) Rickard Nordenberg
ÅAC Microtec
PM: Dr. Fredrik Bruhn
Industry
US Air Force Research Laboratory (AFRL)
PM: Dr. Benjamin “Kyle” Henderson
AFRL/Space Vehicles Directorate
Tech: Dr. James Lyke
US-Sweden bi-lateral agreement on miniaturized aerospace systems and plug-and-play
• August 2009-August 2011
* Bi-lateral Project Agreement (PA-TRDP-US-SW-AF-09-002)
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 8
Rapid Integration Architecture in short
� Self organizing networks according to Space Plug-and-Play Avionics
electronic
Driver
electronicDatasheet /
Driver
Remote Terminal Unit (RTU) orAppliqué Sensor Interface Module (ASIM)
RIA enabled component
driverdriver
USB interface chip
Personal Computerplatform
Driver loaded by Operating
system based on matching unique
device ID
Subsystem / Function
RIAComponent
withDistributed datasheet /
driver (XTEDS)
Driver stored locally in
subsystem and sent to On-board
Computer for parsing
plug-and-playComponent
withUnique ID
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 9
Space Plug-and-Play Avionics
ÅAC Rapid Integration Architecture development kit front-panel
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 10
Write your RIA drivers in no time!
� Generate drivers from standardized Common Data Dictionary
� Verify driver integrity with xml schemas
� Graphically represent driver development
� Fully compatible with USAF Space Plug-and-Play Avionics (SPA)
<?xml version="1.0" encoding="utf-8" ?><xTEDSxmlns="http://www.interfacecontrol.com/SPA/xTEDS" lns:xsi="http://www.w3.org/2001/XMLSchema-instance” xsi:schemaLocation="http://www.interfacecontrol.com/SPA/xTEDS ../Schema/xTEDS02.xsd“name="TemperatureSensor" version="1.0“>
<Device name="TemperatureSensor" kind=“TempSensor" serialNumber ="1295432A" /><Interface name="TemperatureData" id="1" description="Data and messages relating to temperature" ><Variable name="TempC" kind="temperature" format="INT16" description="temp in celsius" units="degC" /><Variable name="TempF" kind="temperature" format="INT16" description="temp in fahrenheit" /><Notification><DataMsg name="TemperatureC" description=“celsius data" id="1" msgArrival="PERIODIC" msgRate="0.25" ><VariableRef name="TempC" /></DataMsg></Notification><Command><CommandMsg name="Reset" description="Re-initializes the temp sensor" id="2" /></Command></Interface></xTEDS>
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 11
You are not alone!
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 12
Swedish-US Space MOU
Implementation Agreement (IA)
Swedish National Space Board (SNSB)
PM: Mr. Christer Nilsson
ÅAC Microtec
Tech: Dr. Fredrik Bruhn
Industry
National Aeronautics & Space Administration (NASA HQ)
PM: Dr. Jitendra Joshi
NASA/Ames Research Center
Tech: Mr. John Hines (Chief Technologist Ames)
Planned US-Sweden bi-lateral agreement on evaluation and cooperation
• May 2011-May 2021
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 13
QuadSat-PnP in-flight qualification setup
� 2 µPOL with 2 µCoil
µPOL 1
µPOL 2
µCoil 1
µCoil 2
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 14
Breaking boundaries, QuadSat-PnP
� 10 kg nanosatellite with active attitude control
PnP Langmuir Probeinstrument(USAF)
PnP SDR NASA TDRS Modem(USAF)
PnP Digital Sun Sensor
Sun detection sensors
8 Solar PanelsSun pointing
Magnetic torquer rod
Magnetic torquer rod
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 15
Breaking boundaries, QuadSat-PnP
ÅAC PnP StarTracker(~10 arcsec)
Size: 250 x 250 mm2
Height: 80 mm
ÅAC PnP 9-DOF INS(3 x Gyro, 3 x Accel, 3 x MGN)
4 x PSLV launch vehicle interface
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 16
ÅAC 2014/15 nanosatellite performance target
� SPAready, Plug-and-play� 6U (30 x 20 x 10) cm3 , < 25 kg� Radhard (> 40 kRAD, SEU free)� ÅAC 32-bit Next Generation CPU on 45/90
nm ASIC CPU technology� 200-400 Mbps SC backbone� >50 Mbps telemetry (LEO)� > 70 W (120 W) Orbit Average Power (OAP)� > 100 GB non-volatile memory� Chip Scale Atomic Clocks (10-12, 125 mW)� 10 arcseconds, 8 Hz lost in space star
tracker� Platform is < 25% of volume, ~ 10% of
power� 20 GFlops� 3 axis stabilized, MTQ, RW
NASA ARC chief technologist, John HinesCenter director, Pete Worden
6U CubeSat form factor
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 17
Advanced science with nanosatellites
Courtesy of NASA. 1.5 m ground resolution F8/1.25m Dobson telescope
Courtesy of NASA. O/OREOS. Astrobiology Nanosatellite Mission.(Organism/Organics Exposure to Orbital Stresses)
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 18
Nominal ModeÅAC PnP OBC
RIA architecture – Prototype a satellite in hours
Main Power Distribution Unit
MPDU
Nominal ModeÅAC PnP OBC
IntersatelliteCommunication
Distributed Power Control UnitDPCU-2112
Distributed Power Control Unit
DPCU-2312/2412
LV-SPA-1 LV-SPA-U/S
LV-SPA-U
System (ACS)
LV-SPA-U (µRTU 312)
Attitude Control System (ACS)
SPA-1 (nanoRTU 212)
Sun Sensor
SPA-1 (nanoRTU 212)
Experiment
SPA-1 (nanoRTU 212)
Experiment
LV- SPA-U (µRTU 312)Star Tracker
AIS receiver
I2C
5 V bus (LV-SPA-5 std)
USB/SpaceWire
TMTC withPulse Commands
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 19
ÅAC Rapid Integration Architecture component summary
ÅAC RIAplatforms
ÅAC RIA Core components
ÅAC Education
Avionics Power Plug’n’Play RIA training
Plug’n’Play RIA educational kits
ThermalQuadSat-PnP
OBC / RTU 800
OBC / RTU lite 500
µRTU 300
DPCU 2100
DPCU 2200
GNC
nanoRTU 200
nanoRTU 200
Non-volatile16 GB MM
Non-volatile16 GB MM
IRSThermalSwitch
DPCU 2300
Virtual Satellite Integration
MPDU 1100
Star Tracker
Sun Sensor
AIO-30
GPS
TT&C
VHF
UHF
L-Band
OrbCOMM
S-band
ÅAC RIAcomponents
Available Q2 2011
Available Q4 2011
In planning
Motion Control
HPC
TDRS
External supplier
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 20
RTU lite 511 with Ethernet add-on
� ÅAC OpenRISC 1200-FT™� DSP, FPU, MMU� CPU 18 MHz� I & D Cache (8 kB/8 kB)� 64 MB SDRAM @ 72 MHz� 8 Gbit NAND Flash� 8 x GPIO TTL� 4 x I2C� 1 x SPI� 1 x USB v1.1� 1 x Ethernet 10/100� 1 x RS 422� 1 x UART TTL� 4 x 12 bit Analog IO� Linux OS
� Dimensions: 34 x 68 mm2
10/100 Ethernet
4 x I2C master/slave
USB 1.1 Host
UART TTL
SPI
GPIOAnalog
IO
Reset button
DebuggerPort
5 V Power
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 21
Conclusions
� Highly capable nano/microsatellites platforms available
� Easy to integrate payloads and support for secure Virtual System Integration (VSI) over internet
� State-of-the-art US/European technologies
� Platform development (cost/risk sharing) possible with Rymdstyrelsen, NASA, FMV, US Air Force, (ESA)
� Estimated production price (excluding payload) for a 6U highly advanced radhard spacecraft, ~ 10-15 million SEK
� 11 nations collaborating on Plug-and-Play. Huge library of easy to use subsystems available in 2015
� ÅAC has the technology today and demonstrating it fully in space in 2012.
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Copyright © ÅAC Microtec AB 2011. www.aacmicrotec.com Page 22
ÅAC Microtec
– Nano/microsatellites and subsystems –
July 2010. Version 1.7
ÅAC Microtec ABDag Hammarskjölds väg 54B,
Uppsala Science ParkSE-751 83 Uppsala, SwedenE: [email protected]
P: +46 18 560130