13-02-2013 дата публикации
Номер: CN102929836A
Принадлежит:
The invention relates to a special ASIC (Application Specific Integrated Circuit) chip system for spaceflight. The special ASIC chip system comprises a MIPS (Million Instructions Per Second) nucleus, a PCI (Programmable Communications Interface) bus interface, an ISA (Internet Security And Acceleration) bus interface, a 1553B bus terminal interface, a 1553B protocol processor, a network interface, a CAN (Controller Area Network) interface, an EMI (External Memory Interface), AD acquisition control logic, OC door control logic, UART (Universal Asynchronous Receiver/Transmitter) serial port, PWM (Pulse Width Modulation) interface, a pulse counter PPC, PCM (Pulse Code Modulation) telemetry remote control module and a general input/output module, wherein the MIPS nucleus, the PCI bus interface, the ISA bus interface, the 1553B bus terminal interface, the 1553B protocol processor, a network interface, the CAN interface and the EMI are connected to an AMBA AXI (Advanced Microcontroller Bus Architecture ...
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