INTEGRATED MISSION COMPUTER HARDWARE SYSTEM FOR CARRYING OUT A MISSION OF HELICOPTER AND METHOD THEREOF

摘要

PURPOSE: An integrated mission computer hardware system and a method thereof for execution of a helicopter are provided to supply an input/output interface and a multichannel graphic for satisfying an operation request condition of a platform. CONSTITUTION: A VME(Versa Module Eurocard)64 bus backplane motherboard(201) supports a bus request, bus permission, and interrupt. A system processor module(202) supplies a VME(Versa Module Eurocard)64-channel graphic generation function to a 1553 multiplexer communication device. A graphic processor module(205) displays various information by supplying a graphic generating function to a multifunctional display device. A digital map processor module(206) installs digital map data and supplies a 2-channel graphic generation function to the multifunctional display device. [Reference numerals] (201) VME64 bus backplane motherboard; (202) System processor module; (205) Graphic processor module; (206) Digital map processor module; (207) Mass memory PMC; (208) Video input/output module(VIOM); (209) Input/output module(IOM); (210) Flight critical Input/Output Module(FIOM); (211) Power Supply Module(PMS); (AA) Graphic PMC(2 channel); (BB) Ethernet channel