DocumentCode
2178354
Title
Ultra-reliable digital avionics (URDA) processor architecture
Author
Branstetter, Reagan ; Harper, Angela ; Denton, Larry
Author_Institution
Defense Syst. & Electron. Group, Texas Instrum. Inc., Dallas, TX, USA
fYear
1994
fDate
23-27 May 1994
Firstpage
274
Abstract
The objective of the URDA program is to develop a prototype advanced development model (ADM) processor that combines a data processor, signal processor, memory and system interface on a single SEM-E avionics card. TI´s approach integrates two Ada-programmable, URDA basic processor modules (BPMs) with a JIAWG-compatible PiBus and TMBus onto a common SEM-E format ADM module and provides a separate, high-speed (25-MWord/s 100-MByte/s) input/output bus for sensor data. Each BPM provides a peak throughput of 100 MIPS scalar concurrent with 400 MFLOPS vector processing in a removable multichip module (MCM). The URDA BPMs use the chipset and BPM architecture developed on the TI Aladdin program to implement a high-performance processor in an MCM package compatible with assembly onto standard form-factor, liquid-flow-through printed wiring board (PWB) modules. A Mips R4000 family reduced instruction set computer (RISC) processor and a TI 100-MHz bipolar complementary metal-oxide semiconductor (BiCMOS) vector co-processor (VCP) application-specific integrated circuit (ASIC) provide, respectively, the 100 MIPS of scalar processor throughput and 400 MFLOPS of vector processing throughput for each BPM. Extensive software development, system modeling and simulation, and system integration and test tools are provided with the URDA processor
Keywords
BiCMOS integrated circuits; aerospace computing; aircraft; aircraft instrumentation; application specific integrated circuits; fault tolerant computing; multichip modules; reduced instruction set computing; reliability; system buses; vector processor systems; 100 MHz; 100 MIPS; 100 Mbyte/s; 400 MFLOPS; Ada; Ada-programmable modules; JIAWG-compatible PiBus; JIAWG-compatible TMBus; Mips R4000 family; RISC; SEM-E avionics card; SEM-E format ADM module; TI Aladdin program; TI BiCMOS vector co-processor; URDA; application-specific integrated circuit; high-performance processor architecture; high-speed input/output bus; prototype advanced development model; reduced instruction set computer; removable multichip module; scalar processor; software development; system interface; ultra-reliable digital avionics; vector processing; Aerospace electronics; Application specific integrated circuits; Assembly; Computer architecture; Integrated circuit packaging; Multichip modules; Prototypes; Semiconductor device packaging; Signal processing; Throughput;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace and Electronics Conference, 1994. NAECON 1994., Proceedings of the IEEE 1994 National
Conference_Location
Dayton, OH
Print_ISBN
0-7803-1893-5
Type
conf
DOI
10.1109/NAECON.1994.332995
Filename
332995
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