DocumentCode :
1642048
Title :
The mast mounted sight 771 processor upgrade program
Author :
Tiberia, L.M.
Author_Institution :
McDonnell Douglas Astronaut. Co., Huntington Beach, CA, USA
fYear :
1989
Abstract :
The 771 microprocessor is used as the main control processor for the Mast Mounted Sight (MMS) on the Bell Helicopter OH-58A helicopter for the US Army Advanced Helicopter Improvement Programme (AHIP). The 771 and its test set/development system were designed in January 1977. These 10-year-old designs currently have a wide range of problems in production, test, and software development. To increase system performance, lower manufacturing costs, and improve software development efforts, an upgraded 771 processor and development system has been developed. The new processor, the 771C, is implemented using ASIC (application-specific integrated circuit) and VLSI technology. The 771C increases memory and I/O capability, reduces board and part counts, and increases throughput by up to 73%. The author describes the 771C and its development system implementation performed at McDonnell Douglas Astronautics Company, Huntington Beach, California.<>
Keywords :
VLSI; aerospace computer control; aircraft instrumentation; application specific integrated circuits; helicopters; microcomputer applications; microprocessor chips; military computing; military equipment; 771C microprocessor control/development system; ASIC; Bell Helicopter OH-58A helicopter; I/O capability; Mast Mounted Sight; McDonnell Douglas Astronautics Company; US Army Advanced Helicopter Improvement Programme; VLSI technology; application-specific integrated circuit; design upgrade; memory increase; software development; Application specific integrated circuits; Circuit testing; Helicopters; Microprocessors; Process control; Production; Programming; Software testing; System performance; System testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Applications Conference, 1989. Digest., 1989 IEEE
Conference_Location :
Breckenridge, CO, USA
Type :
conf
DOI :
10.1109/AERO.1989.82410
Filename :
82410
Link To Document :
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