Microprocessor applications in future aerospace systems
Institute of Electrical and Electronics Engineers. Dayton Section, IEEE Aerospace and Electronic Systems Society
Institute of Electrical and Electronic Engineers, 1981 - Computers - 59 pages
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addressing modes aerospace systems Air Force airborne computer aircraft analog computer application software assembly language avionics avionics computer avionics system Bendix bit slice block diagram buses byte capability channel chip concept configuration Control CPU control scheme data bus device digital control direct memory access distributed processing DMA Controller Dual Port Memory EH-L2 control EH-L2 processor electronic control EM-Cl engine control Fault Tolerant flexibility flight control system Flight Dynamics Flight Dynamics Laboratory functions future hardware and software I/O Controller IEEE implemented input input/output instruction set architecture Intel M^FCS micro microprocessor technology mode modular Multi-Microprocessor Flight Control Multiprocessor Orbiter output perform Portable Module Tester problems program status reconfiguration reduced redundancy management Regional processor registers requirements SCMP Sensor processor sensor remote terminals serial servo processors shown in Figure Shuttle subsystems SYSTEM ARCHITECTURE system design tasks test system throughput tion turbine engine uniprocessor vectored interrupts