| 摘要 |
A computer control system, especially for flight control comprises a series of computer modules FEU operating parallel and asynchronously to carry out respective ports of an overall control algorithm for a series of control functions. Each module FEU has a data transmission port I/L1, 2 etc. connected by a broadcast line to a respective input port of each other computer module. Communication between the modules is thereby achieved by any module broadcasting asynchronous data messages onto its broadcast line enabling messages to be received by any other module which requires them. <IMAGE> |
