The SpaceWire RTC: Remote Terminal Controller

Size: px
Start display at page:

Download "The SpaceWire RTC: Remote Terminal Controller"

Transcription

1 SpaceWire-SnP Working Group ESTEC, Sept 15 th, 2004 The : Remote Terminal Controller Data Systems Division luca.tunesi@esa.int ESTEC, Sept 15 th, 2004 slide: 1

2 Background: the OPDPS Low/Med. Speed Bus:CAN High Speed Network: SpaceWire Inst. 1 Data Compression High Capacity Memory Inst. 2 V, I, T Acquisition (Monitor) Inst. n Discrete Commands RTC Complex Instrument Complex Instrument SpaceWire RTC Telemetry Formatter/ Encryption Instrument RTC I/O Module (Optional) µp Control Processor DSP Processor ESTEC, Sept 15 th, 2004 slide: 2 Spacecraft Control Bus

3 Background: Network Hierarchy SpaceWire High Speed Network Interconnections among systems Interconnections among modules 1Mbit/s Low Speed Bus Low Data rate Instruments bus CAN Telemetry Collection & Commands distribution Data Rate Sensor Bus TBD (1-wire?) Local Sensors bus Debug and Test at Sub-unit level ESTEC, Sept 15 th, 2004 slide: 3

4 Objective A Smart Component for Dumb Terminals Development of an ASIC SpW Remote Terminal Controller (RTC) for connection of SpaceWire nodes (with or without local intelligence)! It shall be Remotely configurable! It shall implement A bridge SpaceWire- CAN! It shall have Some processing power to work autonomously! It will be used for Simple nodes (I/O Boards, TM/TC boards, sensors, actuators) Intelligent nodes such as processor boards, DPUs, ICUs etc. ESTEC, Sept 15 th, 2004 slide: 4

5 Features (1 st st )! Unit configurable and controlled via SpW link (Remote Control)! SpaceWire I/F as high speed links! FIFO (buffer) I/F! RAM (buffer) I/F! CAN I/F Controller (CANC)! RTC Manager embedded µcontroller (RTM) SpW-SnP! GP-I/O configurable channels Digital commands Pulse commands Digital states ESTEC, Sept 15 th, 2004 slide: 5

6 Features (2 nd nd )! ADC Interface for analogue acquisitions! DAC interface! Host bus I/F! Embedded UARTs! Embedded user s Timers! JTAG port for test purposes (TBC) ESTEC, Sept 15 th, 2004 slide: 6

7 Block Diagram Serial links Discrete commands & Status UART 1 UART 2 GP I/O RTC RTC Remote Terminal Controller TIMER 1 DM (Memory) DAC I/F ADC TIMER 2 JTAG RTM RTC Manager (µc) PM (Memory) ADC I/F DAC SpaceWire Interface FIFO/RAM I/F HOST I/F CANC CAN Controller SpaceWire Links FIFO/RAM PROM µp CAN Bus ESTEC, Sept 15 th, 2004 slide: 7

8 Technology! ASIC Process Implementation in ATMEL Rad-hard 0,18µm CMOS process ESA-ATMEL MPWP Multi-Project Wafer Programme Max gate count 7Mgates Standard-cell ATC18RHA libraries! Radiation Tolerance Functional TID up to 200KRads SEU free cells (>100MeV) Used for all critical memory cells Latch-up immunity to >100MeV ESTEC, Sept 15 th, 2004 slide: 8

9 Preliminary Assessment! Technology (TBC) Pad/Pin count: pads, pins Gate Count: 700K-1M gates Reticule M2 (ATC18RHA95_324) or M3 (ATC18RHA95_404)! Performance SpaceWire 200Mbit/s (2links) CAN 1Mbit/s 115.2Kbit/s Processing power TBD! Power Supply/Consumption 1.8V & 3.3V (TBC) mW WC Power consumption (TBC) ESTEC, Sept 15 th, 2004 slide: 9

10 Work Breakdown Structure ESTEC, Sept 15 th, 2004 slide: 10

11 Time Frame! Invitation to Tender Q1 2004! Negotiation On-going! Kick-off Q4 2004! FPGA Prototype Q3 2005! ASIC Prototypes Q2 2006! ATMEL Standard Production Q (TBC) ESTEC, Sept 15 th, 2004 slide: 11

12 Possible Evolution! Field / Sensor Bus (1-wire? )! Integrated smart Sensors! Integrated diagnostic I/F (JTAG like?)! Other I/Fs (MIL-STD-1553?, Wireless ) ESTEC, Sept 15 th, 2004 slide: 12

13 References I., Philippe Armbruster, On-board Hierarchical Network, SPIE 2003 Barcelona (Sp), 8-10 Sept 2003 II. III. Philippe Armbruster, On-board Payload Data Processing Systems, Technical Dossier on Mapping, TOS-E-1A-DOS-1, Issue 1 Revision F, 06 Feb 2003 ESA/ESTEC/TOS-EDP, SpaceWire Web Site, IV. EMITS: ESTEC, Sept 15 th, 2004 slide: 13

Network on Chip round table European Space Agency, ESTEC Noordwijk / The Netherlands 17 th and 18 th of September 2009

Network on Chip round table European Space Agency, ESTEC Noordwijk / The Netherlands 17 th and 18 th of September 2009 Network on Chip round table European Space Agency, ESTEC Noordwijk / The Netherlands 17 th and 18 th of September 2009 Ph. Armbruster Head of Data Systems Division European Space Agency - ESTEC 17 th of

More information

The SMCS332SpW and SMCS116SpW: Development Status

The SMCS332SpW and SMCS116SpW: Development Status SpaceWire-SnP Working Group ESTEC, Sept 15 th, 2004 The SMCS332SpW and SMCS116SpW: Development Data Systems Division luca.tunesi@esa.int What is the SMCS? SMCS (Scalable Multi-channel Communication Sub-system)!

More information

ATMEL SPACEWIRE PRODUCTS FAMILY

ATMEL SPACEWIRE PRODUCTS FAMILY ATMEL SPACEWIRE PRODUCTS FAMILY Session: Components Short Paper Nicolas RENAUD, Yohann BRICARD ATMEL Nantes La Chantrerie 44306 NANTES Cedex 3 E-mail: nicolas.renaud@atmel.com, yohann.bricard@atmel.com

More information

SPACE PACEWIRE STANDARD AND RELATED PRODUCTS FOR THE PAYLOAD DATA HANDLING SYSTEM OF BEPI

SPACE PACEWIRE STANDARD AND RELATED PRODUCTS FOR THE PAYLOAD DATA HANDLING SYSTEM OF BEPI f D document title/ titre du document D O C U M E N T SPACE PACEWIRE STANDARD AND RELATED PRODUCTS FOR THE PAYLOAD DATA HANDLING SYSTEM OF BEPI EPICOLOMBO prepared by/préparé par TOS-EDP reference/réference

More information

SpaceWire Remote Terminal Controller

SpaceWire Remote Terminal Controller Remote Terminal Controller Presented by Jørgen Ilstad On board Payload Data Section, ESTEC Wahida Gasti, ESA ESTEC Co Authors Sandi Habinc, Gaisler Research Peter Sinander, SAAB Space Slide : 1 Overview

More information

On-Board Data Systems

On-Board Data Systems On-Board Data Systems Ph. Armbruster TEC-ED Email: philippe.armbruster@esa.int Slide : 1 Avionics for multi-mission platforms, hard Facts Avionics take an important share of the platform cost Many building

More information

Advanced Concepts and Components for adaptive Avionics

Advanced Concepts and Components for adaptive Avionics Advanced Concepts and Components for adaptive Avionics Ph. Armbruster Head of Data Systems Division ESTEC 03/03/2016 AVIONICS : Cost reduction as a challenge AVIONICS include: Data Handling TM/TC Attitude

More information

Processor and Peripheral IP Cores for Microcontrollers in Embedded Space Applications

Processor and Peripheral IP Cores for Microcontrollers in Embedded Space Applications Processor and Peripheral IP Cores for Microcontrollers in Embedded Space Applications Presentation at ADCSS 2010 MESA November 4 th, 2010 www.aeroflex.com/gaisler Presentation outline Microcontroller requirements

More information

SpaceWire Router ASIC

SpaceWire Router ASIC SpaceWire Router ASIC Steve Parkes, Chris McClements Space Technology Centre, University of Dundee Gerald Kempf, Christian Toegel Austrian Aerospace Stephan Fisher Astrium GmbH Pierre Fabry, Agustin Leon

More information

SpaceWire Router - Status

SpaceWire Router - Status Router - Status Working Group Meeting Dr. Stephan Fischer Dr. Steve Parkes Gerald Kempf Pierre Fabry EADS Astrium GmbH University of Dundee Austrian Aerospace GmbH ESA ESA, Noordwijk 15. Sep. 004 Outline

More information

Microcontrollers Applications within Thales Alenia Space products

Microcontrollers Applications within Thales Alenia Space products ADCSS 2010 Microcontrollers for Embedded Space Applications (MESA) Roundtable Template reference : 100181670S-EN Microcontrollers Applications within Thales Alenia Space products Presented by: M.L. Esposti

More information

GR712RC A MULTI-PROCESSOR DEVICE WITH SPACEWIRE INTERFACES

GR712RC A MULTI-PROCESSOR DEVICE WITH SPACEWIRE INTERFACES GR712RC A MULTI-PROCESSOR DEVICE WITH SPACEWIRE INTERFACES Session: SpaceWire Components Short Paper Sandi Habinc, Jiri Gaisler Aeroflex Gaisler, Kungsgatan 12, SE-411 19 Göteborg, Sweden sandi@gaisler.com

More information

SMCSlite and DS-Link Macrocell Development

SMCSlite and DS-Link Macrocell Development and DS-Link Macrocell Development Microelectronics Final Presentation Days, ESTEC, 6-7 March 2001 Anja Christen Tim Pike Paul Rastetter Astrium GmbH, D-81663 Ottobrunn Tel. ++49-89-60720267, Fax ++49-89-60721302

More information

SpaceWire IP Cores for High Data Rate and Fault Tolerant Networking

SpaceWire IP Cores for High Data Rate and Fault Tolerant Networking SpaceWire IP Cores for High Data Rate and Fault Tolerant Networking E. Petri 1,2, T. Bacchillone 1,2, N. E. L Insalata 1,2, T. Cecchini 1, I. Del Corona 1,S. Saponara 1, L. Fanucci 1 (1) Dept. of Information

More information

Video Processing Chain VPC2 SpaceWire Networking Protocol Meeting July 2005

Video Processing Chain VPC2 SpaceWire Networking Protocol Meeting July 2005 Video Processing Chain VPC2 SpaceWire Networking Protocol Meeting 4 19-20-21 July 2005 Page 1 Summary VPC2 and SPADA_RT Activity VPC2 Architecture Data Exchange VPC2 RMAP Implementation Issue FPGA Implementation

More information

Development an update. Aeroflex Gaisler

Development an update. Aeroflex Gaisler European SpaceWire Router Development an update Sandi Habinc Aeroflex Gaisler Demand for SpaceWire Router Both European and international customers have shown interest in SpaceWire router with greater

More information

Multi-DSP/Micro-Processor Architecture (MDPA)

Multi-DSP/Micro-Processor Architecture (MDPA) Multi-DSP/Micro-Processor Architecture (MDPA) Microelectronics Presentation Days 2010 30 March 2010, ESA/ESTEC, Noordwijk T. Helfers; E. Lembke; P. Rastetter; O. Ried Astrium GmbH Content Motivation MDPA

More information

LEON3-Fault Tolerant Design Against Radiation Effects ASIC

LEON3-Fault Tolerant Design Against Radiation Effects ASIC LEON3-Fault Tolerant Design Against Radiation Effects ASIC Microelectronic Presentation Days 3 rd Edition 7 March 2007 Table of Contents Page 2 Project Overview Context Industrial Organization LEON3-FT

More information

John Cornforth (1), Andrew Bacon (1), I Sturland (2), Roland Trautner (TO) (3) (1) Presented by John Cornforth

John Cornforth (1), Andrew Bacon (1), I Sturland (2), Roland Trautner (TO) (3) (1) Presented by John Cornforth Smart Microsystems A Feasibility Study to Investigate the Decentralisation of Space Systems with highly efficient Micronodes using advanced ASIC technologies John Cornforth (1), Andrew Bacon (1), I Sturland

More information

PowerPC- based Processor Modules for Space Applications

PowerPC- based Processor Modules for Space Applications PowerPC- based Processor Modules for Space Applications Patria Systems OY Jaakko Toivonen 12.09.2006 PowerPC- based Single Board Computers Two Single Board Computer (SBC) modules targeted for space applications:

More information

Advanced Computing, Memory and Networking Solutions for Space

Advanced Computing, Memory and Networking Solutions for Space Advanced Computing, Memory and Networking Solutions for Space 25 th Microelectronics Workshop November 2012 µp, Networking Solutions and Memories Microprocessor building on current LEON 3FT offerings UT699E:

More information

Next Generation Microprocessor for Power Systems Control September 2006 M. Ruiz, SABCA, Belgium

Next Generation Microprocessor for Power Systems Control September 2006 M. Ruiz, SABCA, Belgium Next Generation Microprocessor for Power Systems Control September 2006 M. Ruiz, SABCA, Belgium 1 Next Generation Microprocessor for Power Systems Control Presentation Overview Scope Microprocessor architecture

More information

Operability and Modularity concepts of future RTUs/RIUs

Operability and Modularity concepts of future RTUs/RIUs Operability and Modularity concepts of future RTUs/RIUs ADCSS2015 Day 3 Thursday 22 October 2015 What is a RTU? The Remote Terminal Unit (RTU) is an Avionics equipment that provides functions such as:

More information

Rad-Hard Microcontroller For Space Applications

Rad-Hard Microcontroller For Space Applications The most important thing we build is trust ADVANCED ELECTRONIC SOLUTIONS AVIATION SERVICES COMMUNICATIONS AND CONNECTIVITY MISSION SYSTEMS Rad-Hard Microcontroller For Space Applications Fredrik Johansson

More information

ATMEL ATF280E Rad Hard SRAM Based FPGA. Bernard BANCELIN ATMEL Nantes SAS, Aerospace Business Unit

ATMEL ATF280E Rad Hard SRAM Based FPGA. Bernard BANCELIN ATMEL Nantes SAS, Aerospace Business Unit ATMEL ATF280E Rad Hard SRAM Based FPGA Bernard BANCELIN ATMEL Nantes SAS, Aerospace Business Unit Overview Atmel FPGA Key Points and Architecture ATF280E Radiation Test Results 2 Overview Atmel FPGA Key

More information

Multi-DSP/Micro-Processor Architecture (MDPA) Paul Rastetter Astrium GmbH

Multi-DSP/Micro-Processor Architecture (MDPA) Paul Rastetter Astrium GmbH Multi-DSP/Micro-Processor Architecture (MDPA) Paul Rastetter Astrium GmbH Astrium ASE2 MDPA for New Generation Processor (NGP) Payload Control Processor MDPA (Multi-DSP/ µprocessor Architecture) features:

More information

ETM-ASIC. Condensed Data Sheet

ETM-ASIC. Condensed Data Sheet DUTH/SRL-SPACE ASICS Document Designation: ETM-Data Sheet condensed ETM-ASIC Condensed Data Sheet Status : For Public Release Version : 1 Rev. : A Date : September 29, 2007 Part: Data Sheet - condensed

More information

Fifth SpaceWire WG Meeting SpaceWire based On-Board-Computer

Fifth SpaceWire WG Meeting SpaceWire based On-Board-Computer Fifth SpaceWire WG Meeting 15. - 17.11.2005 SpaceWire based On-Board-Computer On Board Computer Concept Page 2 OBC Concept -Aims- Based on ERC32 32-bit processor cores Fully redundant Each function provided

More information

Essential TeleMetry (ETM) support ASIC

Essential TeleMetry (ETM) support ASIC March 31, 2010 Rationale & Goals ETM Project Rationale/Goals Motivation ETM ASIC Overall Functionality What is currently available? Essential Telemetry Encoding and Telecommand Decoding capability already

More information

Microelectronics Presentation Days March 2010

Microelectronics Presentation Days March 2010 Microelectronics Presentation Days March 2010 FPGA for Space Bernard Bancelin for David Dangla Atmel ASIC BU Aerospace Product Line Everywhere You Are Atmel Radiation Hardened FPGAs Re-programmable (SRAM

More information

Payload Data Processing Technologies for JUICE

Payload Data Processing Technologies for JUICE Payload Data Processing Technologies for JUICE JUICE instrument Workshop ESOC, 9 th -11 th November 2011 R. Trautner, TEC-EDP 1 Contents Presentation Overview Expected payload data processing requirements

More information

Scalable Sensor Data Processor Development Status DSP Day - September 2014

Scalable Sensor Data Processor Development Status DSP Day - September 2014 Scalable Sensor Data Processor Development Status DSP Day - September 2014 83230347-DOC-TAS-EN-003 Presentation of the SSDP ASIC Program & Context SSDP will be the first Space Qualified European multi-core

More information

SpaceWire 101 Seminar MAPLD 2006 SpaceWire origins and purpose From IEEE 1355 to ECSS-E-50-12A

SpaceWire 101 Seminar MAPLD 2006 SpaceWire origins and purpose From IEEE 1355 to ECSS-E-50-12A SpaceWire 101 Seminar MAPLD 2006 SpaceWire origins and purpose From IEEE 1355 to ECSS-E-50-12A Ph. Armbruster TEC-ED Head of Data Systems Division ESA/ESTEC Slide : 1 Contents A little bit of History Transputers

More information

COMPARISON BETWEEN GR740, LEON4-N2X AND NGMP

COMPARISON BETWEEN GR740, LEON4-N2X AND NGMP Doc..: Date: 2017-08-22 Page: 1 of 11 COMPARISON BETWEEN GR740, LEON4-N2X AND NGMP Doc..: Date: 2017-08-22 Page: 2 of 11 TABLE OF CONTENTS 1 INTRODUCTION... 3 1.1 Scope of the Document... 3 1.2 Reference

More information

FPGAs APPLICATIONS. 2012, Sept Copyright Atmel Corporation

FPGAs APPLICATIONS. 2012, Sept Copyright Atmel Corporation FPGAs For SPACE APPLICATIONS 2012, Sept. 1 2012 Copyright Atmel Corporation 03/14/2012 Roadmap Legend Product Eng Sample Concept Eng Sample FM FM AT40K family ATF5000 ATF2500 ATFSee900 Next generation

More information

GOES-R SpaceWire Implementation

GOES-R SpaceWire Implementation GOES-R SpaceWire Implementation William Anderson GSFC/MEI Technologies Inc. William.H.Anderson@nasa.gov International SpaceWire Conference 2007 Dundee, Scotland, UK September 17, 2007 1 GOES-R SpaceWire

More information

Next Generation Multi-Purpose Microprocessor

Next Generation Multi-Purpose Microprocessor Next Generation Multi-Purpose Microprocessor Presentation at MPSA, 4 th of November 2009 www.aeroflex.com/gaisler OUTLINE NGMP key requirements Development schedule Architectural Overview LEON4FT features

More information

MPW Program for Space ESA Contract: 17767/03/NL/FM. Jean BOUILLON MDP ESA Feb 4th, 2004

MPW Program for Space ESA Contract: 17767/03/NL/FM. Jean BOUILLON MDP ESA Feb 4th, 2004 MPW Program for Space ESA Contract: 17767/03/NL/FM Jean BOUILLON MDP ESA Feb 4th, 2004 MPW Space Objectives! For ATC18RHA ASIC family! Share the set of reticules and silicon costs between several designs!

More information

A ONE CHIP HARDENED SOLUTION FOR HIGH SPEED SPACEWIRE SYSTEM IMPLEMENTATIONS

A ONE CHIP HARDENED SOLUTION FOR HIGH SPEED SPACEWIRE SYSTEM IMPLEMENTATIONS A ONE CHIP HARDENED SOLUTION FOR HIGH SPEED SPACEWIRE SYSTEM IMPLEMENTATIONS Joseph R. Marshall, Richard W. Berger, Glenn P. Rakow Conference Contents Standards & Topology ASIC Program History ASIC Features

More information

RAD6000 Space Computers

RAD6000 Space Computers RAD6000 Space Computers RAD6000 space computers RAD6000 single-board computers combine commercial standards with unique radiation-hardened technology and packaging to meet the specific requirements of

More information

Command & Data Handling. By: Justin Hadella Brandon Gilles

Command & Data Handling. By: Justin Hadella Brandon Gilles Command & Data Handling By: Justin Hadella Brandon Gilles Outline Design Goals Requirements System Layout Processor Considerations Baseline Design Current Development 2 Design Goals 1 Watt Operational

More information

Massively Parallel Processor Breadboarding (MPPB)

Massively Parallel Processor Breadboarding (MPPB) Massively Parallel Processor Breadboarding (MPPB) 28 August 2012 Final Presentation TRP study 21986 Gerard Rauwerda CTO, Recore Systems Gerard.Rauwerda@RecoreSystems.com Recore Systems BV P.O. Box 77,

More information

ESA round table. September L. Goulard PY. Bretécher

ESA round table. September L. Goulard PY. Bretécher Next generation processors for space ESA round table September 2006 L. Goulard PY. Bretécher Agenda Brief history of processors used at Sodern On going developments AT697E evaluation Requirement review

More information

1 COMMAND AND DATA HANDLING (C&DH)

1 COMMAND AND DATA HANDLING (C&DH) 1 COMMAND AND DATA HANDLING (C&DH) 1.1 Requirements and Design Drivers 1.1.1 Functional The command and data handling shall provide the capability to: Transfer information in digital or discrete representation

More information

11th symposium on advanced space technologies in robotics and automation

11th symposium on advanced space technologies in robotics and automation 11th symposium on advanced space technologies in robotics and automation CONTRIBUTION OF A POWERFUL IMAGE PROCESSING UNIT TO THE AUTONOMY OF ROBOTIC INSTRUMENTS Thomas Würgler, Neuchâtel, Switzerland Thursday,

More information

ATF280E A Rad-Hard reprogrammable FPGA

ATF280E A Rad-Hard reprogrammable FPGA ATF280E A Rad-Hard reprogrammable FPGA ESA/ESTEC 3 rd Microelectronics Presentation Days 2007 Valérie Ho-Shui-Ling Thibaud Gaillard Overview ATMEL rad-hard FPGA family The ATF280E FPGA ATMEL FPGA architecture

More information

Radiation Tolerant Digital I/O Module KM6784.1

Radiation Tolerant Digital I/O Module KM6784.1 Radiation Tolerant Digital I/O Module KM6784.1 MAIN FEATURES Power Consumption: 1W Digital I/O: Discrete signals SpaceWire: 3x UARTS with RS422: 6x Dimensions: 160x100 mm 2 (Europe Card Size) Mass: 0.32

More information

Building Blocks For System on a Chip Spacecraft Controller on a Chip

Building Blocks For System on a Chip Spacecraft Controller on a Chip PIO/TEST/WDOGN/ 19 ERRORN 2 Clock, Reset CT_PULSE CT_EVENT 4 4 4 SWB0 : Space Wire SWB1 : Space Wire SWB2 : Space Wire HKP Housekeeping Packetizer Context RA CT CCSDS Time anager SWT SWITCH ATRIX IT from

More information

ENHANCED DYNAMIC RECONFIGURABLE PROCESSING MODULE FOR FUTURE SPACE APPLICATIONS

ENHANCED DYNAMIC RECONFIGURABLE PROCESSING MODULE FOR FUTURE SPACE APPLICATIONS Enhanced Dynamic Reconfigurable Processing Module for Future Space Applications ENHANCED DYNAMIC RECONFIGURABLE PROCESSING MODULE FOR FUTURE SPACE APPLICATIONS Session: SpaceWire Missions and Applications

More information

The Essential Telemetry (ETM) ASIC A mixed signal, rad-hard and low-power component for direct telemetry acquisition and miniaturized RTU

The Essential Telemetry (ETM) ASIC A mixed signal, rad-hard and low-power component for direct telemetry acquisition and miniaturized RTU DUTH/SRL SPACE-ASICS The Essential Telemetry (ETM) ASIC A mixed signal, rad-hard and low-power component for direct telemetry acquisition and miniaturized RTU G. Kottaras 1, E. Sarris 2, A. Psomoulis 2,

More information

The special radiation-hardened processors for new highly informative experiments in space

The special radiation-hardened processors for new highly informative experiments in space Journal of Physics: Conference Series PAPER OPEN ACCESS The special radiation-hardened processors for new highly informative experiments in space To cite this article: O V Serdin et al 2017 J. Phys.: Conf.

More information

Development Status for JAXA Critical Parts, 2008

Development Status for JAXA Critical Parts, 2008 The 21st Microelectronics Workshop Development Status for JAXA Critical Parts, 2008 Oct. 7th 2008 Electronic Components and Devices Group Aerospace Research and Development Directorate, JAXA Hiroyuki SHINDOU

More information

Plug and Play Satellite Evolution

Plug and Play Satellite Evolution Plug and Play Satellite Evolution AIAA/USU Conference On Small Satellites August, 2009 SSC09-VI-4 Don Fronterhouse PnP Innovations, Inc SPA Genealogical Tree Adaptive Avionics Experiment Responsive Space

More information

European LVDS Driver Development and ESCC Evaluation and Qualification

European LVDS Driver Development and ESCC Evaluation and Qualification European LVDS Driver Development and ESCC Evaluation and Qualification Aeroflex Gaisler AB Kungsgatan 12, SE-41119 Gothenburg, Sweden info@gaisler.com +46 31 775 86 50 1 Quick introduction ESA Contract

More information

AT697E LEON2-FT Final Presentation

AT697E LEON2-FT Final Presentation AT697E LEON2-FT Final Presentation ESA contract 15036/01/NL/FM Nicolas RENAUD ATMEL Nantes + 33 2 40 18 17 19 nicolas.renaud@nto.atmel.com Overview Initial objectives design phase Validation and characterisation

More information

September 16, ESA/ESTEC - Data Systems Division. Low Speed Multidrop Busses - New. Architectures Enabled by All-Digital Low Speed

September 16, ESA/ESTEC - Data Systems Division. Low Speed Multidrop Busses - New. Architectures Enabled by All-Digital Low Speed Bus Bus /ESTEC - Data Systems Division September 16, 2008 1 / 16 Bus Bus 1 2 Bus The architecture Where do we already use digital busses The Transducer Bus What do we gain? 3 It is not just chat 4 2 /

More information

Overview of Microcontroller and Embedded Systems

Overview of Microcontroller and Embedded Systems UNIT-III Overview of Microcontroller and Embedded Systems Embedded Hardware and Various Building Blocks: The basic hardware components of an embedded system shown in a block diagram in below figure. These

More information

Executive Summary. Functional and Performance Validation of the 80S32 µc. Deliverable D5.2 - Report Workpackage 5 Evaluation Kit

Executive Summary. Functional and Performance Validation of the 80S32 µc. Deliverable D5.2 - Report Workpackage 5 Evaluation Kit Functional and Performance Validation of the 80S32 µc Executive Summary Deliverable D5.2 - Report Workpackage 5 Evaluation Kit Author(s): T.Lampaounas, C.Papadas, E.Politis, G.Dramitinos, K.Makris Reviewer(s):

More information

ESA Supported General Purpose Standard Microprocessors

ESA Supported General Purpose Standard Microprocessors ESA Supported General Purpose Standard Microprocessors MPSA Roundtable on Microprocessors for Space Applications ESTEC, 04 November 2009 Roland Weigand European Space Agency Roland.Weigand[at]esa.int (1)

More information

HIGH PERFORMANCE ELECTRONICS FOR THE NEW SPACE AGE

HIGH PERFORMANCE ELECTRONICS FOR THE NEW SPACE AGE APP18-01c APPLICATION NOTE NOVO SPACE HIGH PERFORMANCE ELECTRONICS FOR THE NEW SPACE AGE INTRODUCTION Most subsystem can be partially or fully implemented using one or more of Novo s components. This document

More information

Reconfigurable System-on-Chip Data Processing Units for Space Imaging Instruments

Reconfigurable System-on-Chip Data Processing Units for Space Imaging Instruments Reconfigurable System-on-Chip Data Processing Units for Space Imaging Instruments B. Fiethe, H. Michalik, C. Dierker, B. Osterloh, G. Zhou IDA TU Braunschweig, Hans-Sommer-Str. 66, D-38106 Braunschweig,

More information

European LVDS driver development and ECSS evaluation and qualification

European LVDS driver development and ECSS evaluation and qualification European LVDS driver development and ECSS evaluation and qualification resenter: Jørgen Ilstad 18 th SpW working group SpW component development ESTEC 25/04/2012 ESA UCLASSIFIED For Official Use ECI phase

More information

SpaceWire IP for Actel Radiation Tolerant FPGAs

SpaceWire IP for Actel Radiation Tolerant FPGAs SpaceWire IP for Actel Radiation Tolerant FPGAs Steve Parkes, Chris McClements Space Technology Centre, University of Dundee Zaf Mahmood Actel UK 1 Actel RTAX-S Devices 2 Radiation tolerant FPGAs Non-volatile

More information

On-Board Control Procedures: Autonomous and Updateable Spacecraft Operator Onboard and Beyond

On-Board Control Procedures: Autonomous and Updateable Spacecraft Operator Onboard and Beyond On-Board Control Procedures: Autonomous and Updateable Spacecraft Operator Onboard and Beyond Marek Prochazka / Kjeld Hjortnaes European Space Agency, ESTEC, Software Systems Division. FSW-10, Pasadena

More information

Dynamically Reconfigurable Processing Module for Future Space Applications

Dynamically Reconfigurable Processing Module for Future Space Applications Dynamically Reconfigurable Processing Module for Future Space Applications Giuseppe Montano, Paul Norridge, Wayne Sullivan, Chris Topping, Alex Wishart Astrium Limited, Gunnels Wood Road, Stevenage, SG1

More information

DSM ASIC Technology & HSSL (KIPSAT)

DSM ASIC Technology & HSSL (KIPSAT) DSM ASIC Technology & HSSL (KIPSAT) Presented by L.Dugoujon ST/APM/MSH Microelectronics Presentation Days ESA/ESTEC 30March-01April 2010. 2 OUTLINE Need for DSM 65nm Key IPs KIPSAT project phases/status

More information

RPWI Software Design SWEDISH INSTITUTE OF SPACE PHYSICS. Reine Gill

RPWI Software Design SWEDISH INSTITUTE OF SPACE PHYSICS. Reine Gill RPWI Software Design SWEDISH INSTITUTE OF SPACE PHYSICS Reine Gill 2012-05-08 Software Environment (Design A, Design B) - Dataflows (Instruments, Spacecraft TM/TC) - Signals (Clocks, Interrupts, Pulse

More information

CAN: from Components to Minisatellites

CAN: from Components to Minisatellites CAN: from Components to Minisatellites COMPANY OVERVIEW 2 A worldwide leading Transportation and Aerospace Group SYNERGIC HIGH-TECH COMPANIES WITH 1000+ HIGHLY SKILLED EMPLOYEES Railway Space Aviation

More information

EMC2. Prototyping and Benchmarking of PikeOS-based and XTRATUM-based systems on LEON4x4

EMC2. Prototyping and Benchmarking of PikeOS-based and XTRATUM-based systems on LEON4x4 EMC2 Prototyping and Benchmarking of PikeOS-based and XTRATUM-based systems on LEON4x4 Introduction Multi-core architectures will be adopted in the next generations of avionics and aerospace systems. Integrated

More information

SpaceWire Remote Memory Access Protocol

SpaceWire Remote Memory Access Protocol SpaceWire Remote Memory Access Protocol Steve Parkes and Chris McClements University of Dundee, Applied Computing, Dundee, DD1 4HN, Scotland, UK. sparkes@computing.dundee.ac.uk,, cmclements@computing.dundee.ac.uk.

More information

LEVERAGING SERIAL DIGITAL INTERFACES STANDARDIZATION: THE RASTA REFERENCE ARCHITECTURE FACILITY AT ESA

LEVERAGING SERIAL DIGITAL INTERFACES STANDARDIZATION: THE RASTA REFERENCE ARCHITECTURE FACILITY AT ESA LEVERAGING SERIAL DIGITAL INTERFACES STANDARDIZATION: THE RASTA REFERENCE ARCHITECTURE FACILITY AT ESA Session: Spacewire onboard equipment and software Short Paper Aitor Viana Sanchez, Gianluca Furano,

More information

Standardisation of PF/PL interfaces TAS point of view

Standardisation of PF/PL interfaces TAS point of view ADCSS-2014 workshop Day 3 ESTEC October 29, 2014 30/10/2014 Standardisation of PF/PL interfaces TAS point of view 83230352-DOC-TAS-EN-002 Ref.: Agenda For Proteus, H/P, Sentinel 3, Telecom, the following

More information

Digital Control for Space Power Management Devices

Digital Control for Space Power Management Devices Template reference : 100182079N-EN Digital Control for Space Power Management Devices Work conducted under ESA Contract nr.21826/08/nl/lvh DIGITAL POWER CONTROL Management of power devices via digital

More information

Mixed Signal ICs for Space

Mixed Signal ICs for Space Power Matters. TM Mixed Signal ICs for Space Microsemi Space Forum 2015 Dorian Johnson Product Marketing Manager High Reliability ICs 1 New Products Legacy Custom Mixed Signal ICs for Space SSM Telemetry

More information

SCS750. Super Computer for Space. Overview of Specifications

SCS750. Super Computer for Space. Overview of Specifications SUPER COMPUTER FOR SPACE TM Super Computer for Space F FLIGHT MODULE Overview of Specifications One board upset every 100 years in a GEO or LEO Orbit Up to 1000X Better Performance Than Current Space Processor

More information

SINGLE BOARD COMPUTER FOR SPACE

SINGLE BOARD COMPUTER FOR SPACE SINGLE BOARD COMPUTER FOR SPACE Proven in Space Best Single Event Performance Seamless Error Correction Wide Range of Processing Power Highest Design Margin SCS750 FLIGHT MODULE Overview of Specifications

More information

VORAGO TECHNOLOGIES. Solutions for Selective Radiation-Hardened Components in CubeSats Ross Bannatyne, VORAGO Technologies

VORAGO TECHNOLOGIES. Solutions for Selective Radiation-Hardened Components in CubeSats Ross Bannatyne, VORAGO Technologies VORAGO TECHNOLOGIES Solutions for Selective Radiation-Hardened Components in CubeSats Ross Bannatyne, VORAGO Technologies rbannatyne@voragotech.com VORAGO Technologies VORAGO Technologies, Austin, Texas.

More information

ESA IPs & SoCs developments

ESA IPs & SoCs developments ESA IPs & SoCs developments Picture courtesy of: Lightwave esearch Laboratory Columbia University NY 1 ESA IP cores portfolio Processor Leon2 FT Fault tolerant Sparc V8 architecture Data handling Interfaces

More information

Product Specification PE95421

Product Specification PE95421 Product Description The PE95421 is an RF SPDT switch available in a hermetically sealed ceramic package and also available in die. It covers a broad range of applications from 1-to-8500 MHz and has been

More information

SpaceFibre Flight Software Workshop 2015

SpaceFibre Flight Software Workshop 2015 SpaceFibre Flight Software Workshop 2015 Steve Parkes, University of Dundee Albert Ferrer Florit, Alberto Gonzalez Villafranca, STAR-Dundee Ltd. David McLaren, Chris McClements, University of Dundee Contents

More information

PROFIBUS-DP to G-64 CONFIGURABLE INTERFACE

PROFIBUS-DP to G-64 CONFIGURABLE INTERFACE EUROPEAN ORGANIZATION FOR NUCLEAR RESEARCH CERN SL DIVISION SL-Note-2001-016 BT PROFIBUS-DP to G-64 CONFIGURABLE INTERFACE E. Carlier, A. Moreno Forrellad # (SL/BT), J. Rochez (IT/CO) and J. Serrano (PS/CO)

More information

Overview of ESA activities on FPGA technology

Overview of ESA activities on FPGA technology Overview of ESA activities on FPGA technology David Merodio Codinachs European Space Agency Microelectronics Section (TEC-EDM) 30 th April 2010 Slide 1/43 Acknowledgments Thanks to all colleagues who contributed

More information

Mixed-Signal. From ICs to Systems. Mixed-Signal solutions from Aeroflex Colorado Springs. Standard products. Custom ASICs. Mixed-Signal modules

Mixed-Signal. From ICs to Systems. Mixed-Signal solutions from Aeroflex Colorado Springs. Standard products. Custom ASICs. Mixed-Signal modules A passion for performance. Mixed-Signal solutions from Aeroflex Colorado Springs Standard products Custom ASICs Mixed-Signal modules Circuit card assemblies Mixed-Signal From ICs to Systems RadHard ASICs

More information

ExoMars Rover Vehicle

ExoMars Rover Vehicle Page: 2 of 21 PAGE INTENTIONALLY LEFT BLANK Page: 3 of 21 TABLE OF CONTENTS 1 INTRODUCTION... 5 1.1 Purpose and Scope... 5 1.2 Priority of requirements... 5 1.3 Guidelines and Traceability... 5 2 DOCUMENTS...

More information

8051 Microcontroller

8051 Microcontroller 8051 Microcontroller The 8051, Motorola and PIC families are the 3 leading sellers in the microcontroller market. The 8051 microcontroller was originally developed by Intel in the late 1970 s. Today many

More information

GR716 Single-Core LEON3FT Microcontroller. Cobham Gaisler AMICSA 2018

GR716 Single-Core LEON3FT Microcontroller. Cobham Gaisler AMICSA 2018 GR716 Single-Core LEON3FT Microcontroller Cobham Gaisler AMICSA 2018 Introduction Description The GR716 features a fault-tolerant LEON3 SPARC V8 processor, communication interfaces and on-chip ADC, DAC,

More information

About using FPGAs in radiation environments

About using FPGAs in radiation environments About using FPGAs in radiation environments Tullio Grassi (FNAL / Univ. of MD) Motivations We may need some "glue logic" between the Front-End ASICs and the GBT (see talk from Chris Tully HB/HE Strawman

More information

OBC Mass Memories Final Presentation

OBC Mass Memories Final Presentation OBC Mass Memories Final Presentation Patrik Sandin, Chief Engineer, Digital Product Unit, AB Dietmar Walter, Hardware Group, DSI-IT GmbH Glenn Johnson, Onboard Software Group, SCISYS UK Ltd ESA Contract

More information

ESA Contract 18533/04/NL/JD

ESA Contract 18533/04/NL/JD Date: 2006-05-15 Page: 1 EUROPEAN SPACE AGENCY CONTRACT REPORT The work described in this report was done under ESA contract. Responsibility for the contents resides in the author or organisation that

More information

SpaceWire ECSS-E50-12A International SpaceWire Seminar (ISWS 2003)

SpaceWire ECSS-E50-12A International SpaceWire Seminar (ISWS 2003) SpaceWire ECSS-E50-12A International SpaceWire Seminar (ISWS 2003) 4-5 November 2003, ESTEC Noordwijk, The Netherlands Steve Parkes (1), Josep Rosello (2) (1) University of Dundee, Applied Computing, Dundee,

More information

32 bit Embedded Real-time computing Core Single Chip Development (ERC32SC/TSC695) Contract 12598/FM (SC)

32 bit Embedded Real-time computing Core Single Chip Development (ERC32SC/TSC695) Contract 12598/FM (SC) 32 bit Embedded Real-time computing Core Single Chip Development (ERC32SC/TSC695) Contract 12598/FM (SC) T. Corbiere, J. Tellier, C. LeGargasson, B. Mouchel, S. Vandepeute, ATMEL WM, France A. Pouponnot,

More information

SpaceWire-RT. SpaceWire-RT Status SpaceWire-RT IP Core ASIC Feasibility SpaceWire-RT Copper Line Transceivers

SpaceWire-RT. SpaceWire-RT Status SpaceWire-RT IP Core ASIC Feasibility SpaceWire-RT Copper Line Transceivers SpaceWire-RT SpaceWire-RT Status SpaceWire-RT IP Core ASIC Feasibility SpaceWire-RT Copper Line Transceivers 1 Overview of SpaceWire-RT Project Aims The SpaceWire-RT research programme aims to: Conceive

More information

TAS RTU PRODUCTS. ADCSS 2015 Noordwijk. Thales Alenia Space 23/10/2015. Ref.: DOC-TAS-EN-001

TAS RTU PRODUCTS. ADCSS 2015 Noordwijk. Thales Alenia Space 23/10/2015. Ref.: DOC-TAS-EN-001 TAS RTU PRODUCTS ADCSS 2015 Noordwijk 83230356-DOC-TAS-EN-001 TAS PRODUCTS & DEVELOPMENT 83230356-DOC-TAS-EN-001 TAS-BELGIUM HIGH POWER AVIONICS Development programme underway under ARTES R&D Modular PLDIU

More information

2-Oct-13. the world s most energy friendly microcontrollers and radios

2-Oct-13.  the world s most energy friendly microcontrollers and radios 1 2 3 EFM32 4 5 LESENSE Low Energy Sensor Interface Autonomous sensing in Deep Sleep LESENSE with central control logic ACMP for sensor input DAC for reference generation Measure up to 16 sensors Inductive

More information

A common basic SW and DPU platform for the JUICE mission Instruments

A common basic SW and DPU platform for the JUICE mission Instruments The most important thing we build is trust ADVANCED ELECTRONIC SOLUTIONS AVIATION SERVICES COMMUNICATIONS AND CONNECTIVITY MISSION SYSTEMS A common basic SW and DPU platform for the JUICE mission Instruments

More information

OPERATIONAL UP TO. 300 c. Microcontrollers Memories Logic

OPERATIONAL UP TO. 300 c. Microcontrollers Memories Logic OPERATIONAL UP TO 300 c Microcontrollers Memories Logic Whether You Need an ASIC, Mixed Signal, Processor, or Peripheral, Tekmos is Your Source for High Temperature Electronics Using either a bulk silicon

More information

Product Specification PE95421

Product Specification PE95421 Product Description The PE95421 is an RF SPDT switch available in a hermetically sealed ceramic package and also available in die. It covers a broad range of applications from 1-to-8500 MHz and has been

More information

A Robust Nanosatellite OBC Created with SEL and SEU Immunity as a Driving Requirement

A Robust Nanosatellite OBC Created with SEL and SEU Immunity as a Driving Requirement A Robust Nanosatellite OBC Created with SEL and SEU Immunity as a Driving Requirement OBC Design Drivers Number of in-house missions requiring a robust 32bit OBCfor on-board data handlingfunction. No existing

More information

SPACEWIRE DRIVEN ARCHITECTURE FOR THE ASTRO-H SATELLITE

SPACEWIRE DRIVEN ARCHITECTURE FOR THE ASTRO-H SATELLITE SPACEWIRE DRIVEN ARCHITECTURE FOR THE ASTRO-H SATELLITE Session: SpaceWire missions and applications Long Paper Masanobu Ozaki, Tadayuki Takahashi, Motohide Kokubun, Takeshi Takashima, Hirokazu Odaka Institute

More information

SpaceWire PC Card Development. Patria New Technologies Oy ESA / ESTEC

SpaceWire PC Card Development. Patria New Technologies Oy ESA / ESTEC SpaceWire PC Card Development Patria New Technologies Oy ESA / ESTEC SpaceWire PC Card Standard type II PC Card (Cardbus( I/F) with two SpaceWire links Access to SpaceWire networks by using a standard

More information