Radiation Tolerant FPGA Update

Similar documents
Radiation Tolerant FPGAs and Space System Managers

Radiation-Tolerant FPGAs Update Space Forum 2017

Radiation-Tolerant FPGAs

Radiation-Tolerant FPGAs

RTG4 Enabled by Microsemi Power Technology Portfolio

Agenda. Programming Qualification for Rad-Tolerant Antifuse FPGAs. RT FPGA Qualification Updates. Long Term Reliability Testing

NEPP Independent Single Event Upset Testing of the Microsemi RTG4: Preliminary Data

Radiation-Tolerant FPGA Update

SEFUW workshop. Feb 17 th 2016

Field Programmable Gate Array (FPGA) Devices

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

HX5000 Standard Cell ASIC Platform

Virtex-II Architecture. Virtex II technical, Design Solutions. Active Interconnect Technology (continued)

A ONE CHIP HARDENED SOLUTION FOR HIGH SPEED SPACEWIRE SYSTEM IMPLEMENTATIONS

8. Migrating Stratix II Device Resources to HardCopy II Devices

16th Microelectronics Workshop Oct 22-24, 2003 (MEWS-16) Tsukuba Space Center JAXA

IGLOO2 Evaluation Kit Webinar

Xilinx Virtex-5QV Update and Space Roadmap Kangsen Huey Space Marketing Aerospace & Defense 17th, March, 2016

Microelectronics Presentation Days March 2010

Basic FPGA Architecture Xilinx, Inc. All Rights Reserved

Microsemi Secured Connectivity FPGAs

Serializer Deserializer POSSIBILITIES OF COMMUNICATION. MADE EASY. For extremely high communications reliability in radiation environments

SmartFusion 2 System-on-Chip FPGA

SpaceWire IP Cores for High Data Rate and Fault Tolerant Networking

SCS750. Super Computer for Space. Overview of Specifications

Advanced Computing, Memory and Networking Solutions for Space

EE178 Lecture Module 2. Eric Crabill SJSU / Xilinx Fall 2007

About using FPGAs in radiation environments

Microsemi Update for SPWG 2017

SmartFusion 2 Next-generation System-on-Chip FPGA Lowest Power Advanced Security Highest Reliability 150K LEs ARM Cortex -M3 DSP Transceivers DDR3

Altera Product Overview. Altera Product Overview

1. Overview for the Arria II Device Family

SINGLE BOARD COMPUTER FOR SPACE

Field Programmable Gate Array (FPGA)

Radiation-Tolerant ProASIC3 Low-Power Space- Flight Flash FPGAs

LEON3-Fault Tolerant Design Against Radiation Effects ASIC

The Fully Configurable Cortex-M3

FPGA VHDL Design Flow AES128 Implementation

Programmable Logic. Any other approaches?

FPGAs APPLICATIONS. 2012, Sept Copyright Atmel Corporation

APEX II The Complete I/O Solution

Mixed Signal ICs for Space

1. Cyclone IV FPGA Device Family Overview

RTG4 PLL SEE Test Results July 10, 2017 Revised March 29, 2018 Revised July 31, 2018

High temperature / radiation hardened capable ARM Cortex -M0 microcontrollers

S950 3U cpci Radiation Tolerant PowerPC SBC

Development an update. Aeroflex Gaisler

Zynq-7000 All Programmable SoC Product Overview

Axcelerator Family FPGAs

Military Grade SmartFusion Customizable System-on-Chip (csoc)

ATF280E A Rad-Hard reprogrammable FPGA

DATA SHEET AGM AG16K FPGA. Low Cost and High Performance FPGA. Revision: 1.0. Page 1 of 17

ADVANCED ELECTRONIC SOLUTIONS AVIATION SERVICES COMMUNICATIONS AND CONNECTIVITY MISSION SYSTEMS

Designing Radiation-Tolerant Power-Supplies for the RTAX-S/SL/DSP FPGA

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

Libero SoC v11.9 SP2 Release Notes 11/2018

Section I. Cyclone II Device Family Data Sheet

Initial Single-Event Effects Testing and Mitigation in the Xilinx Virtex II-Pro FPGA

1. Overview for the Arria V Device Family

ESA-CNES Deep Sub-Micron program ST 65nm. Laurent Dugoujon Remy Chevallier STMicroelectronics Grenoble, France.

HX5000 ASIC Platform S150 (150 nm) ASICs

ispgdx2 vs. ispgdx Architecture Comparison

Stratix. Introduction. Features... Programmable Logic Device Family. Preliminary Information

Section I. Cyclone II Device Family Data Sheet

Section I. Device Core for Arria II Devices

GOES-R SpaceWire Implementation

8. Selectable I/O Standards in Arria GX Devices

Ultra-low power, Single-chip SRAM FPGA Targets Handheld Consumer Applications

Programmable Logic Devices FPGA Architectures II CMPE 415. Overview This set of notes introduces many of the features available in the FPGAs of today.

Microsemi Corporation: CN18002

Stratix. Introduction. Features... 10,570 to 114,140 LEs; see Table 1. FPGA Family. Preliminary Information

Current status of SOI / MPU and ASIC development for space

MAX 10 FPGA Device Overview

The High-Reliability Programmable Logic Leader. Products for Space Applications. QML Certification Part of Overall Quality Platform

S2C K7 Prodigy Logic Module Series

Space: The Final Frontier FPGAs for Space and Harsh Environments

Aeroflex Colorado Springs RadHard Eclipse FPGA Frequently Asked Questions

DSM ASIC Technology & HSSL (KIPSAT)

6. I/O Features for HardCopy IV Devices

3. Mapping Stratix III Device Resources to HardCopy III Devices

GR712RC A MULTI-PROCESSOR DEVICE WITH SPACEWIRE INTERFACES

Qsys and IP Core Integration

PowerPC- based Processor Modules for Space Applications

Section I. Cyclone II Device Family Data Sheet

ESE532: System-on-a-Chip Architecture. Today. Message. Graph Cycles. Preclass 1. Reminder

DATA SHEET. Low Cost and High Performance FPGA. Revision: 1.1. Release date: Page 1 of 18

Intel MAX 10 FPGA Device Overview

ATMEL SPACEWIRE PRODUCTS FAMILY

Interfacing FPGAs with High Speed Memory Devices

Summary. Introduction. Application Note: Virtex, Virtex-E, Spartan-IIE, Spartan-3, Virtex-II, Virtex-II Pro. XAPP152 (v2.1) September 17, 2003

Intel Cyclone 10 GX Device Overview

RAD6000 Space Computers

Optimal Management of System Clock Networks

6. I/O Features in Stratix IV Devices

INTRODUCTION TO FIELD PROGRAMMABLE GATE ARRAYS (FPGAS)

CSP: HIGH PERFORMANCE RELIABLE COMPUTING FOR SMALLSATS

Stratix. High-Density, High-Performance FPGAs. Available in Production Quantities

Section I. Cyclone FPGA Family Data Sheet

1. Stratix IV Device Family Overview

MAX 10 FPGA Device Overview

Transcription:

Radiation Tolerant FPGA Update Ken O Neill Director of Marketing, Space and Aviation Microsemi SOC Group MRQW January 28, 2015 2015 Microsemi Corporation.. 1

Agenda Current Status In-Service Radiation Tolerant FPGAs Next-Generation FPGA for Space Applications Qualification Plans Conclusion and Next Steps 2014 Microsemi Corporation. 2

In-Service RT FPGAs Update RTSX-SU Over 2,000 SEU-hardened flip flops EAR controlled, no longer ITAR Flight heritage since 2005 RTAX-S/SL/DSP Over 20,000 SEU-hardened flip flops Over 500kbits on-board SRAM Up to 120 multiply-accumulate blocks EAR controlled, no longer ITAR Flight heritage since 2007 Mars Reconnaissance Orbiter RTSX-SU on board (2005) Cosmo Skymed 1 4 RTAX on board (2007) RT ProASIC3 First Flash-based FPGA in space Reprogrammable and non-volatile EAR controlled, no longer ITAR Now QML class Q qualified NASA IRIS RT ProASIC3 on board (2013)

TM Next Generation Radiation-Tolerant FPGAs 2014 Microsemi Corporation..

RT FPGAs Migrating to High Speed Processing Logic Density 150 KLE 20 KLE RTAX-S / DSP Command and Control Medium Speed Processing High Speed Processing 150 KLE 5 Mbit SRAM 126 GMults / second 75 Gbit / second SERDES bandwidth 9 KLE RT ProASIC3 2 KLE RTSX-SU Frequency of Operation 2014 Microsemi Corporation. 5

Next Generation Space FPGAs Designed for high-bandwidth data processing in payload applications Abundant high-performance programmable logic fabric Embedded high speed multiply-accumulate blocks Ample on-board memory with fast access time, two block sizes High performance I/Os SERDES, LVDS, DDR2, Based on 65nm Flash low power process Naturally resistant to configuration upsets Non-volatile configuration live at power-up, no external boot memory needed Low static power RTG4 radiation enhanced for GEO and deep space Total ionizing dose, Single event effects, Latch-up immunity 2015 Microsemi Corporation.. 6

RTG4 Family Resources RT4G075 RT4G150 RT4G200 LUT4 + TMR/SET FF 77,712 151,824 202,896 User IO (non-serdes) 528 720 816 RAM24K Blocks 111 209 269 uram1.5k Blocks 112 210 270 RAM Mbits 2.8 5.2 6.7 UPROM Kbits 254 381 417 18x18 Multiply-Accumulate Blocks 224 462 594 SERDES lanes 16 24 32 DDR2/3 SDRAM Controller (with ECC) 2x32 2x32 2x32 Globals 24 24 24 PLLs (Rad Tolerant) 8 8 8 Spacewire Clock & Data Recovery Circuits 12 12 12 PCI Express Endpoints 2 2 2 Packages CG1432 CG1657 CG2092 2015 Microsemi Corporation. 7

Radiation Specifications Total Dose > 100 KRad TID Single Event Effects No configuration failures (to be tested to > 110 MeV-cm 2 /mg) No single event latch-up (to be tested to > 110 MeV-cm 2 /mg) Mitigation for single event upsets Flip-flops with TMR and asynchronous self-correction (LET TH > 37 MeV-cm 2 /mg) Flip-flops in the logic fabric Flip-flops in embedded features Mathblocks etc On-chip SRAM (RAM24K and uram1.5k) Built-in EDAC 1E-10 errors/bit-day, GEO solar min Mitigation of single event transients Logic cells hardened with SET filter SET filter can be individually enabled / disabled for higher performance Target 1E-8 errors/bit-day, GEO solar min 2015 Microsemi Corporation.. 8

TID Mitigation in RTG4 Flash FPGAs Traditional Sense-Switch interconnect V T changes as device accumulates TID Results in T PD increase Example RT ProASIC3 has 10% T PD degradation at around 30Krad RTG4 TID - Tolerant interconnect Accumulation of TID causes V T changes in PFG and NFG floating-gate devices However, interconnect pass transistor stays strongly turned on as long as PFG is stronger than NFG Minimal change in T PD with accumulated TID to > 100Krad 2015 Microsemi Corporation.. 9

RT4G150 Device Floorplan 2 CCC 2 PLL DDR CALIB CCC -EIPS Serial Sub-system EIP-Clusters CCC -EIPS 2 CCC 2 PLL DDR CALIB SERDES, PCS, PCI-Express Logic Cells Mathblocks DDRIOs Bank L1 MSIODs Bank L2 FDDR Controller IIP (LSRAM, usram, Math) IIP (LSRAM, usram, Math) Clock VS IIP (LSRAM, usram, Math) IIP-Clusters Clock HS IIP (LSRAM, usram, Math) Clock VS IIP (LSRAM, usram, Math) IIP (LSRAM, usram, Math) Factory Segment and User Segment BL ACCESS FDDR Controller DDRIOs Bank R1 HVGEN MSIODs Bank R2 SDRAM DDRx Controller Block RAM (24Kb) μram (1.5Kb) MSIODs Bank L3 2 CCC 2 PLL CCC -EIPS MSIOs Bank B1 Clock VS IIP-Clusters IO-Clusters uproms WL ACCESS MSIOs Bank B2 Clock VS uprom- EIPS MSIOs Bank B3 CCC -EIPS Bank J1 JTAG and SPI pins RTG4 Control MSIODs Bank R3 2 CCC 2 PLL PLL and CCC 2015 Microsemi Corporation. 10

RTG4 Logic Module TMR Protected Simplified Diagram Dedicated STMR Flip-flop to enable efficient TMR hardening With enable, global asynchronous set/reset, and local synchronous set/reset Fast carry chain to complement Mathblock performance Arithmetic functions (add/subtract) Target 300 MHz for 32-bit functions (no SET filter) Target 250 MHz for 32-bit function (SET filter deployed) Industry standard LUT4 for efficient synthesis High utilization LUT4 and flip-flop in same module can be used independently Hierarchical routing architecture enables >95% module utilization 2015 Microsemi Corporation. 11

RTG4 Mathblock A[17:0] D ADD_SUB EN B[17:0] D + X D OVFL / CO S N [43:0] EN D[43:0] EN C[43:0] D SHIFT17 D >> 17 EN EN SEL_CASC S N-1 [43:0] 18 x 18 multiplier with advanced accumulate New 3-input adder function: (C + D) +/- (A * B) High performance for signal processing throughput 250 MHz with SET mitigation 300 MHz without SET mitigation Optional SEU-protected registers on inputs and outputs (including C input) 2015 Microsemi Corporation. 12

RTG4 Memory Blocks Radiation Tolerant Resistant to multi-bit upset Built-in optional EDAC (SECDED) LSRAM up to 24 KBit Dual-port and two-port options High performance synchronous operation Example usage Large FFT memory uram up to 1.5 KBit Three Port Memory Synchronous Write Port Two Asynchronous or Synchronous Read Ports Example usage Folded FIR filters and FFT twiddle factors Mixed port sizes Write and read port sizes can be different 300 MHz performance CLKA ADDRA[ ] WDATAA[17:0] WENA CLKB ADDRB[ ] WDATAB[17:0] WENB WCLK WADDR[ ] WDATA[17:0] WEN RCLKA RADDRA[ ] RENA RCLKB RADDRB[ ] RENB RAM24K uram1.5k RDATAA[17:0] ECC_STATA RDATAB[17:0] ECC_STATB RDATAA[17:0] ECC_STATA RDATAB[17:0] ECC_STATB 2015 Microsemi Corporation. 13

General Purpose IO Single ended standards LVCMOS from 1.2V to 3.3V LVTTL PCI Voltage reference standards (600+ Mbps) Includes on-chip termination SSTL2, SSTL18 and SSTL15 For DDR2/DDR3 SDRAM memories HSTL18 and HSTL15 For SRAM memories Differential I/O standards Includes on-chip termination True LVDS (600+ Mbps) Mini-LVDS, M-LVDS, RSDS, LVPECL 2015 Microsemi Corporation. 14

SpaceWire Hardened Clock Recovery Selected from pad_ccc_clk<3:0> Data Strobe D MUX S MUX dmux#_out smux#_out Delay Cell rxclk<#> To Global Clock Network Rx Recovery sel_rx_#<3:2> sel_rx_#<1:0> del_sel<4:0> Data and Strobe can connect to LVDS or LVTTL input pins Optional Single Event Transient filtering 2015 Microsemi Corporation. 15

3.125Gbps SERDES PMA Based on PCIe Gen 1 PHY RT Performance = 1 3.125 Gbps Up to eight x4 units PCI Express Protocol x1, x2, x4 64-bit AXI /AHB PCI Express Interface 4 X16 PIPE 8B/10B Encoding / Decoding PCS Programmable Logic TXDn RXDn 1 PMA 4 x 20-bit EPCS SRIO Or Custom Protocol Serializer / Deserializer Clock Recovery XAUI Bridge XGMII 802.3 Or Custom Protocol <= 3.125GHz <= 156MHz 2015 Microsemi Corporation. 16

Performance Summary General purpose logic 250 MHz system performance with SET mitigation deployed 300 MHz system performance without SET mitigation 300 MHz DSP support performance (adders, delays, etc.) Mathblock 250 MHz pipelined performance with SET mitigation deployed 300 MHz pipelined performance without SET mitigation RAM18K and uram1k > 300 MHz IO > 600 Mbps LVDS and 667 Mbps DDRx SDRAM data SERDES to 3.125 Gbps Overall 250 MHz general system performance with SET mitigation deployed 300 MHz signal processing performance without SET mitigation 2015 Microsemi Corporation. 17

RTG4 Packaging Summary Flip chip assembly Hermetically-sealed cavity Internally-mounted BME decoupling capacitors Thermal adhesive between die and seal lid (passed RGA <5,000ppm, passed outgas to NASA spec) BME decoupling capacitors placed inside Kovar Lid RTG4 Die Under fill (passed RGA <5,000ppm, passed outgas to NASA spec) 2015 Microsemi Corporation. 18

RTG4 Product Availability RT devices for space flight applications Initial device: RT4G150 Early access to software and documents via Lead Customer Program: NOW Sample RT4G150 silicon: March 2015 RT4G150 development kit: April 2015 Mil Std 883 class B flight units: 1Q CY2016 QML class Q qualification: 4Q CY2016 QML class V qualification: 2017 RTG4 Lead Customer Program Start product evaluation and provide feedback Early access software: NOW RTG4 user guides: NOW Power calculator: NOW Open to new participants send email to RTG4_LCP@microsemi.com 2015 Microsemi Corporation. 19

Qualification Plans Mil Std 883 Class B qualification Starts 4 th quarter, CY2015 Completes 1 st quarter, CY2016 Qualification will use RT4G150 in CG1657 packages 3 wafer lots 3 assembly lots 1,000 hour HTOL QML class Q qualification Technology insertion package currently in preparation phase Intent is to achieve QML-Q by end of CY2016 QML class V qualification It is our intention to achieve QML class V Working with DLA, SMC / Aerospace, NASA, JPL to ensure requirements are clear and understood 2015 Microsemi Corporation.. 20

RTG4 Conclusions and Next Steps Non-volatile RT FPGA for payload data processing High density, high performance, low power RTG4 FPGA Lead customer program with software access NOW Sample RT4G150 silicon: March 2015 RT4G150 development kit: April 2015 Mil Std 883 class B flight units: 1Q CY2016 QML class Q qualification: 4Q CY2016 Next steps Mil Std 883 class B qualification: 1Q CY2016 QML class Q qualification: 4Q CY2016 QML class V qualification: 2017 2015 Microsemi Corporation. 21

Microsemi Space Forum Detailed discussions on Microsemi space products discrete, power, RF, ASIC, FPGA, timing Space product roadmap Design tips and tricks Qualification and reliability updates Radiation testing results and mitigation strategies Package development and roadmap Development and verification tools Downloads at http://www.microsemi.com/spaceforum Next events June 2015 USA (Los Angeles, Washington DC area) June 2015 Europe (Noordwijk, Netherlands) August 2015 India (Bangalore, Ahmedabad) 2015 Microsemi Corporation. 22