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RECONFIGURABLE PROCESSING AND AVIONICS SYSTEMS

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Presentation on theme: "RECONFIGURABLE PROCESSING AND AVIONICS SYSTEMS"— Presentation transcript:

1 RECONFIGURABLE PROCESSING AND AVIONICS SYSTEMS
RUSS DUREN DEPARTMENT OF ENGINEERING Duren 1

2 RECONFIGURABLE COMPUTING
Duren 2

3 WHAT IS RECONFIGURABLE COMPUTING?
STANDARD COMPUTERS PERFORM DIFFERENT TASKS BY CHANGING THE PROGRAM THAT THE COMPUTER EXECUTES RECONFIGURABLE COMPUTERS ARE PROGRAMMED BY CHANGING THE HARDWARE THAT EXECUTES THE PROGRAM TYPICALLY RECONFIGURABLE COMPUTERS DO BOTH STANDARD PROGRAMS ARE EXECUTED BY A STANDARD PROCESSOR RECONFIGURABLE HARDWARE IS USED TO ACCELERATE CRITICAL PORTIONS OF THE CODE RECONFIGURABLE HARDWARE IS IMPLEMENTED USING FIELD PROGRAMMABLE GATE ARRAYS (FPGAs) Duren 3

4 XILINX FIELD PROGRAMMABLE GATE ARRAYS
I/O Blocks (IOBs) Programmable Interconnect Configurable Logic Blocks (CLBs) Special Purpose Resources Duren 4

5 CONFIGURABLE LOGIC BLOCKS (CLBs)
BASIC RESOURCE UNIT IS THE SLICE 1 CLB CONTAINS 4 LOGIC CELLS SLICE = 4-INPUT LOOK-UP TABLE (LUT) + D FLIP-FLOP LUT CAPACITY LIMITED BY NUMBER OF INPUTS, NOT COMPLEXITY OF FUNCTION LUTS CAN BE USED AS LOGIC, RAM, OR ROM LUT FF Duren 5

6 Signed Multiply Performance
ADDITIONAL RESOURCES INPUT/OUTPUT BLOCKS (IOBS) PROGRAMMABLE INTERCONNECT DELAY-LOCKED LOOPS (DLLS) BLOCK RAM FAST CARRY LOGIC MULTIPLIERS XC2V6000 VIRTEX II FPGA 33,792 SLICES 2,592 Kbits of BLOCK RAM bit MULTIPLIERS AT 140 MHz > 25 BILLION MULTIPLIES/SEC 18 Bit 36 Bit 8 x 8 210MHz 4 x 4 255MHz 12 x 12 170MHz 18 x 18 140MHz Signed Multiply Performance Preliminary V1.60 Speeds File Duren 6

7 PROCESSING SPEED IMPROVEMENTS
RECONFIGURABLE COMPUTERS USE FPGAS TO INCREASE PROCESSING SPEED BY: USING CUSTOM HARDWARE TO COMPUTE RESULTS QUICKLY USING PARALLEL CIRCUITRY TO COMPUTE MULTIPLE ANSWERS SIMULTANEOUSLY USING PIPELINING TO INCREASE THROUGHPUT ASSEMBLY LINE COMPUTATIONS LATENCY THROUGHPUT Duren 7

8 Microprocessor Chassis
SRC-6E Microprocessor Chassis MAP Chassis Duren 8

9 SRC-6E mP Chassis mP Chassis MAP Chassis Duren 9 P3 mP P3 mP P3 mP
(1000 MHz) P3 mP (1000 MHz) P3 mP (1000 MHz) P3 mP (1000 MHz) 800* 800* 8000 8000 MAP Chassis Cache Cache Cache Cache 800 Controller Controller 800 MIOC MIOC 4800 (6 x 800) 4800 (6 x 800) PCI-X Slots SNAP On-Board Memory (24 MB) On-Board Memory (24 MB) SNAP PCI-X Slots Memory (1.5 GB) Memory (1.5 GB) 4800 (6 x 800) 4800 (6 x 800) User Logic User Logic User Logic User Logic 2400 2400 * Peak Theoretical 315 MB/s Write 195 MB/s Read Duren 9

10 MAP Dual Processor Chain Port Board 18in x 13in Duren 10 Chain Port
Control Logic DMA engine Controls User Logic User Logic 2 Virtex II - 6M gates each 100-MHz clock Chain Port MAP/SNAP Cable Connectors On-Board Memory 6 dual-ported memory banks 24M bytes 64b data paths Board 18in x 13in Duren 10 Chain Port

11 SRC-6E PROGRAMMING ENVIRONMENT
PENTIUM PROCESSORS LINUX OPERATING SYSTEM IS THE MAIN USER INTERFACE C AND FORTRAN COMPILERS FOR CODE DEVELOPMENT INTEL AND GNU COMPILERS SUPPORTED FPGAS SRC-6E CUSTOM COMPILER CONVERTS HLL TO FPGA CIRCUITRY FPGA ROUTINES WRITTEN IN C OR FORTRAN SOFTWARE GENERATES ONE EXECUTABLE RESULT Duren 11

12 HARDWARE COMPILER SRC COMPILER TRANSLATES THE C SOURCE INTO PIPELINED FPGA CIRCUITRY FPGAS ARE CLOCKED AT 100 MHz ONCE THE PIPELINE IS FILLED (LATENCY) RESULTS ARE PRODUCED EVERY 10 NANOSECONDS IMPLEMENTS PARALLEL CIRCUITRY FOR INDEPENDENT STATEMENTS A(n) = my_func(X(n),Y(n)) A(n+1) = my_func(X(n+1),Y(n+1)) A(n+2) = my_func(X(n+2),Y(n+2)) A(n+3) = my_func(X(n+3),Y(n+3)) Duren 12

13 LIMITATIONS IMPOSED ON HLL ROUTINES
VERSION 1.3 SUPPORTS: DATA TYPES: 32-BIT (INT) AND 64-BIT (LONG LONG) ADD, SUBTRACT, MULTIPLY DIVISION (32-BIT ONLY) RELATIONAL OPERATORS (==, !=, <, >, <=, >=) BITWISE OPERATORS AND SHIFTS (&, |, !, <<, >>) LOGICAL OPERATORS (&&, !, ||) SQRT() (32BIT ONLY) SOME RESTRICTIONS ON VARIABLE ACCESS AND CONTROL STATEMENTS NOT PARTICULARLY LIMITING, BUT MUST BE CONSIDERED EXAMPLE: NUMBER OF DATA WORDS TRANSFERRED MUST BE MULTIPLE OF 4 FUTURE VERSIONS OF THE COMPILER WILL SUPPORT MORE OPERATIONS AND DATA TYPES AND RELAX RESTRICTIONS Duren 13

14 RECONFIGURABLE RESEARCH TOPICS
APPLICATION DEVELOPMENT FOR SRC-6E FOR MULTIPLE FPGAS PLATFORM COMPARISON SRC, STARBRIDGE, WILDFIRE, NASA CLUSTER WITH FPGA NODES ALGORITHM CLASSIFICATION WHAT ALGORITHMS ARE BEST SUITED TO FPGA? MATCHING ALGORITHMS TO ARCHITECTURES AND VICE VERSA COMBINING ADAPTABLE HARDWARE WITH ADAPTABLE ALGORITHMS NEURAL NETWORKS, GENETIC ALGORITHMS DESIGN OF A CUSTOM RECONFIGURABLE PLATFORM Duren 14

15 AVIONICS SYSTEMS Duren 15

16 Duren 16

17 Federated Avionics System
HUD MPD KEYPAD HOTAS DISPLAY CONTROLLER SMS STORES MISSION COMPUTER 1 INS/GPS RADAR/ SENSORS COMMS MIL-STD-1553 Data Bus MISSION COMPUTER 2 FLIGHT CONTROLS EW SYSTEMS DATA LINK Federated Avionics System Duren 17

18 AVIONICS RESEARCH TOPICS
DATA COMPRESSION ROUTINES FOR REAL-TIME, EMBEDDED, DEMAND-OPERATED SYSTEMS SURVEY OF DATA TYPES AND TRANSMISSION RATES SELECTION OF POTENTIAL COMPRESSION ROUTINES ANALYSIS OF POTENTIAL BANDWIDTH SAVINGS REAL-TIME SYSTEM ANALYSIS AND MODELING EMERGING TOOLS FOR AVIONICS ARCHITECTURE MODELING AND ANALYSIS SYSTEM OF SYSTEMS RESEARCH: HOW TO TAKE ADVANTAGE OF NETWORKED SYSTEMS EXAMPLE: COMBAT ID - TARGET DETECTION, IDENTIFICATION, TRACKING, ELIMINATION OF MULTIPLE REPORTS Duren 18

19 RECONFIGURABLE AVIONICS SYSTEMS
Duren 19

20 RECONFIGURABLE SATELLITE AVIONICS
NAVAL POSTGRADUATE SCHOOL CFTP PROGRAM LAUNCHES SEPTEMBER 2006 PC-104 IBM PERSONAL COMPUTER CUSTOM RECONFIGURABLE PROCESSOR BOARD DEMONSTRATE COMMERCIAL, OFF-THE-SHELF FPGA TECHNOLOGY APPLIED TO SPACECRAFT ARCHITECTURE AS A MEANS OF DECREASING DEVELOPMENT TIME DECREASING COSTS INCREASING FLEXIBILITY AND RELIABILITY Duren 20

21 Configurable Fault Tolerant Processor
Duren 21

22 NPS Configurable Fault Tolerant Processor (CFTP)
EDAC voter memory I/O Status TRIPLE-REDUNDANT, FAULT-TOLERANT RECONFIGURABLE SYSTEM-ON-A-CHIP (SOC) DESIGN TO MITIGATE BIT ERRORS IN COMPUTATION BY DETECTING ERRORS AND CORRECTING THEM THROUGH VOTING LOGIC Duren 22

23 RECONFIGURABLE SPACE AVIONICS
RESEARCH OPPORTUNITIES FAILURE ANALYSIS ON CURRENT DESIGN ADDITIONAL EXPERIMENTS FOR RECONFIGURABLE BOARD ERROR DETECTION ERROR CORRECTION FAULT TOLERANT CIRCUITS PARTIAL FPGA RECONFIGURATION TECHNIQUES FOR REMOTE DEBUGGING OF HARDWARE Duren 23


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