LIGHT MULTIPURPOSE AIRCRAFT WITH A CONTROL INTEGRATED SYSTEM

摘要

Inventive aircraft comprises a fuselage (1), a wing (2), fins (3), a landing gear (4) and an engine unit (5).The aircraft also comprises a navigation system, integrated control systems, an electronic display system, an emergency escape system, an objective inspection system, a common aircraft equipment system, a targeting designator system, an information input system, a speech information-and-control system, control boards, an airborne communication system, airborne maintenance monitors and an integrated control facility (6). Said integrated control facility comprises an airborne digital computer system (7) and an information exchange system consisting of multiplexer and radial channels. The airborne digital computer system (7) communicates through interface systems and/or units with the aircraft systems, including the common aircraft equipment system, by means of the multiplexer channels. Said common aircraft equipment system (23) consists of converting and computing units (27, 28), which are connected to a control unit (29), and of interface units for connecting to the common aircraft equipment system. The converting and computing units (27, 28) are connected to the multiplexer information exchange channel, and the control unit (29) communicates by means of the radial channels with the interface units of the common aircraft equipment system and the other aircraft systems, which are also connected to the multiplexer or radial channels of the control integrated facility (6) system. The invention increases the efficiency to carry out the control and diagnosis functions of all the system of the aircraft.