®. ® Rad Hard Products for Satellites and Space ® www.xilinx.com QPRO for Avionics  Standard QPRO products immune to upsets in avionics environment.

Slides:



Advertisements
Similar presentations
10 December 2012 Clive Max Maxfield All Programmable FPGAs, SoCs, and 3D ICs Part V. Advanced Concepts and Future Trends 1.
Advertisements

IHP Im Technologiepark Frankfurt (Oder) Germany IHP Im Technologiepark Frankfurt (Oder) Germany ©
C3 / MAPLD2004Lake1 Radiation Effects on the Aeroflex RadHard Eclipse FPGA Ronald Lake Aeroflex Colorado Springs.
Scrubbing Approaches for Kintex-7 FPGAs
Discussion of: “Terrestrial-based Radiation Upsets: A Cautionary Tale” CprE 583 Tony Kuker 12/06/05.
Multi-Bit Upsets in the Virtex Devices Heather Quinn, Paul Graham, Jim Krone, Michael Caffrey Los Alamos National Laboratory Gary Swift, Jeff George, Fayez.
Xilinx Space Heritage Jeff Wetch Aerospace and Defense
Radiation Effects on FPGA and Mitigation Strategies Bin Gui Experimental High Energy Physics Group 1Journal Club4/26/2015.
The NSEU Sensitivity of Static Latch Based FPGAs and Flash Storage CPLDs Joseph Fabula Jason Moore Austin Lesea Saar Drimer MAPLD2004 This work has benefited.
MURI Neutron-Induced Multiple-Bit Upset Alan D. Tipton 1, Jonathan A. Pellish 1, Patrick R. Fleming 1, Ronald D. Schrimpf.
Complex Upset Mitigation Applied to a Re-Configurable Embedded Processor EEL 6935 Lu Hao Wenqian Wu.
1 Fault Tolerant FPGA Co-processing Toolkit Oral defense in partial fulfillment of the requirements for the degree of Master of Science 2006 Oral defense.
Radiation Tolerance D. C. Christian, J. A. Appel, G. Chiodini,
April 30, Cost efficient soft-error protection for ASICs Tuvia Liran; Ramon Chips Ltd.
ICAP CONTROLLER FOR HIGH-RELIABLE INTERNAL SCRUBBING Quinn Martin Steven Fingulin.
Microprocessor Reliability
DC/DC Switching Power Converter with Radiation Hardened Digital Control Based on SRAM FPGAs F. Baronti 1, P.C. Adell 2, W.T. Holman 2, R.D. Schrimpf 2,
Reconfigurable Computers in Space: Problems, Solutions and Future Directions Neil W. Bergmann, Anwar S. Dawood CRC for Satellite Systems Queensland University.
Maintaining Data Integrity in Programmable Logic in Atmospheric Environments through Error Detection Joel Seely Technical Marketing Manager Military &
March 16-18, 2008SSST'20081 Soft Error Rate Determination for Nanometer CMOS VLSI Circuits Fan Wang Vishwani D. Agrawal Department of Electrical and Computer.
Danish Space Research Institute Danish Small Satellite Programme FH Space_Environment.ppt Slide # 1 Flemming Hansen MScEE, PhD Technology Manager.
MAPLD99 Total Dose and SEE of Metal-To-Metal Antifuse FPGA.
Estimation of SEUs in the FPGAs C. Targett-Adams V. Bartsch, M. Wing M. Warren, M. Postranecky.
Submission 1003Baranski1 Reliability Studies on Aeroflex’s RadHard ViaLink TM PROM Brian Baranski, Anthony Jordan, and Craig Hafer Aeroflex Colorado Springs.
Radiation Effects and Mitigation Strategies for modern FPGAs 10 th annual workshop for LHC and Future experiments Los Alamos National Laboratory, USA.
12004 MAPLD: 141Buchner Single Event Effects Testing of the Atmel IEEE1355 Protocol Chip Stephen Buchner 1, Mark Walter 2, Moses McCall 3 and Christian.
MAPLD 2005 / E134 Rockett A 0.15  M Radiation-Hardened Antifuse Field Programmable Gate Array Technology The RH AX250-S production installation effort.
144_C4 / MAPLD04Swift and Roosta1 Tradeoffs in Flight-Design Upset Mitigation in State-of-the-Art FPGAs Hardened By Design vs. Design-Level Hardening Gary.
Platform ASICs Reliability Bob Madge Miguel Vilchis LSI Logic, Milpitas, CA Vish Bhide.
A comprehensive method for the evaluation of the sensitivity to SEUs of FPGA-based applications A comprehensive method for the evaluation of the sensitivity.
Presented by Anthony B. Sanders NASA/GSFC at 2005 MAPLD Conference, Washington, DC #196 1 ALTERA STRATIX TM EP1S25 FIELD-PROGRAMMABLE GATE ARRAY (FPGA)
Reconfiguration Based Fault-Tolerant Systems Design - Survey of Approaches Jan Balach, Jan Balach, Ondřej Novák FIT, CTU in Prague MEMICS 2010.
J. Christiansen, CERN - EP/MIC
® SPARTAN Series High Volume System Solution. ® Spartan/XL Estimated design size (system gates) 30K 5K180K XC4000XL/A XC4000XV Virtex S05/XL.
Cypress Roadmap: Aerospace Memory
The Continued Evolution of Re-Configurable FPGAs for Aerospace and Defense Strategic Applications Howard Bogrow.
2/2/2009 Marina Artuso LHCb Electronics Upgrade Meeting1 Front-end FPGAs in the LHCb upgrade The issues What is known Work plan.
MAPLD 2005/202 Pratt1 Improving FPGA Design Robustness with Partial TMR Brian Pratt 1,2 Michael Caffrey, Paul Graham 2 Eric Johnson, Keith Morgan, Michael.
Mil/Aero Logic for the 21 st Century The Future is Programmable High Reliability Products Committed to Leadership.
1 The NSEU Sensitivity of Static Latch Based FPGAs and Flash Storage CPLDs Joseph Fabula Jason Moore Austin Lesea Saar Drimer MAPLD2004 This work has benefited.
®. ® H Defense H Avionics H Space FPGAs For High-Reliability Applications PRODUCTS.
29 May 2008 Exploration Technology Development Program’s Radiation Hardened Electronics for Space Environments (RHESE) Andrew S. Keys, James H. Adams,
Upgrade Radiation Issues Christopher O’Grady For the DCH Electronics Upgrade Group Based on work by Jerry Va’vra.
14/Sept./2004 LECC2004 Irradiation test of ASIC and FPGA for ATLAS TGC Level-1Trigger System 1 TID (  -ray) and SEE (proton) tests and results for ROHM.
A NEUTRON IRRADIATION DEVICE FOR THE TESTING OF MICROELECTRONIC COMPONENETS TO BE USED IN THE RADIATION ENVIRONMENT OF HIGH-ENERGY PARTICLE ACCELERATORS.
COTS for the LHC radiation environment: the rules of the game
In-Place Decomposition for Robustness in FPGA Ju-Yueh Lee, Zhe Feng, and Lei He Electrical Engineering Dept., UCLA Presented by Ju-Yueh Lee Address comments.
2004 MAPLD, Paper 1008 Sanders 1 Radiation-Hardened re-programmable Field- Programmable Gate Array (RHrFPGA) A.B. Sanders 1, K.A. LaBel 1, J.F. McCabe.
Presented by Anthony B. Sanders NASA/GSFC at 2004 MAPLD Conference, Washington, DC April 27-29, Radiation-Hardened re-programmable Field- Programmable.
Nishinaga No. 1 MAPLD2005/1003-J Availability Analysis of Xilinx FPGA on Orbit Nozomu Nishinaga National Institute of Information and Communications Technology.
®. ® H Defense H Avionics H Space FPGAs For High-Reliability Applications PRODUCTS.
Ketil Røed - LECC2005 Heidelberg Irradiation tests of the ALICE TPC Front-End Electronics chain Ketil Røed Faculty of Engineering, Bergen University.
Xilinx V4 Single Event Effects (SEE) High-Speed Testing Melanie D. Berg/MEI – Principal Investigator Hak Kim, Mark Friendlich/MEI.
MAPLD 2005/213Kakarla & Katkoori Partial Evaluation Based Redundancy for SEU Mitigation in Combinational Circuits MAPLD 2005 Sujana Kakarla Srinivas Katkoori.
Ketil Røed University of Bergen - Department of Physics Ketil Røed MSc student, microelectronics University of Bergen Norway Irradiation tests of Altera.
Presenter Dr. Brock J. LaMeres Associate Professor
Rad (radiation) Hard Devices used in Space, Military Applications, Nuclear Power in-situ Instrumentation Savanna Krassau 4/21/2017 Abstract: Environments.
Electrical Engineering Dept.
Problems and solutions to the use of FPGA's in radiation zones
CFTP ( Configurable Fault Tolerant Processor )
SEU Mitigation Techniques for Virtex FPGAs in Space Applications
Upgrade of the ATLAS MDT Front-End Electronics
Radiation Tolerance of an Used in a Large Tracking Detector
Maintaining Data Integrity in Programmable Logic in Atmospheric Environments through Error Detection Joel Seely Technical Marketing Manager Military &
Design of a ‘Single Event Effect’ Mitigation Technique for Reconfigurable Architectures SAJID BALOCH Prof. Dr. T. Arslan1,2 Dr.Adrian Stoica3.
Upset Susceptibility and Design Mitigation of
Xilinx Kintex7 SRAM-based FPGA
Rad Hard Products for Satellites and Space
FPGAs For High-Reliability Applications
Presentation transcript:

®

® Rad Hard Products for Satellites and Space

® QPRO for Avionics  Standard QPRO products immune to upsets in avionics environment  Extensive neutron SEU testing performed - Stability of device storage cells prevents upsets - Readback feature allows user to verify data in the configuration latches  No reported instance of alpha particle induced soft error - Polyimide coating provides effective barrier

® Neutron Testing Results Single-Event Upset  Devices Tested XC4010E (5V) 178,096 SRAM-bits XC4010XL (3.3V)283,376 SRAM-bits  Irradiated with 100MeV cyclotron neutron energy  SEU Rate at aircraft altitude (~30,000 Ft.) XC4010E: 1 bit error per 600,000 flight hours (68.5 years) XC4010XL: 1 bit error per 125,000 flight hours (14.3 years)  No Latch-up

® Major Avionics Customer Conclusion “SRAM-based FPGAs (Xilinx XC4000 series) show a low susceptibility to single event upsets caused by high energy neutrons…… we conclude that these SRAM-based FPGAs can be used without limitation in the atmospheric radiation environment, contrary to large SRAM memories where precaution in the use is necessary because of neutron-induced SEU.“

® Rad Hard Products  Only Re-Configurable Rad Hard FPGA  Manufactured on QML line, special epi process  Utilize same geometries as non-rad Hard QML devices to facilitate prototyping  Guaranteed radiation specs  Densities up to 1M system gates with Virtex

® IC Process  Advanced CMOS process enhanced with epitaxial layer – 0.35um for XQR4000XL – 0.22um for Virtex – 7um epitaxial substrate

® Radiation Specifications  Total Ionizing Dose – XQR4000XL = 60Krads(si) – Virtex = 100Krads(si) – QA monitor on every wafer lot  Latch-up Immune LET th >120 MeV*cm o C  Low Soft Upset Rates

® Total Dose Testing  Testing performed at McClellan AFB, Sacramento, CA. – Cobalt-60 source – Per MIL-STD-883, Method – Dose rate of 50rads/sec  Irradiated parts tested to full production test program

® XQR4000XL Family Product PackageSystem GatesAvailable XQR4013XL-3 CB228 10K to 30K Now XQR4036XL-3 CB228 20K to 65K Now XQR4062XL-3 CB228 40K to 130K Now

® Virtex Rad Hard Family ProductPackageSystem GatesAvailable XQVR300-4 CB ,000 Q200 XQVR600-4 CB ,000Q300 XQVR CG560 1,000,000Q200

® Rad Hard SPROMs

® Radiation Hardened Product/Process Roadmap  0.25  0.35  XQR4000XL Virtex 13K to 62K Gates 150K to +1M Gates Virtex E Product Introduced 62K gates XQVR Radiation testing completed Introduction 2Q00 1M gates >1M gates

® Space Programs Designed With QPRO Rad Hard Products  Litton Amecom (miniaturized satellite receiver)  JPL (Mars 2003 lander and rover vehicle)  Draper Labs (fault tolerant computer for Shuttle program)  Los Alamos Labs (reconfigurable computer)  Canadian Space Agency (satellite instrumentation)  Raytheon (satellite transponder)  Applied Physics Lab (reconfigurable instrumentation module)  Spar Aerospace (communications satellite)  Alcatel (communications satellite)  Spectrum Astro (GPS for military satellites)