LIGHT MULTIPURPOSE AIRCRAFT

摘要

The inventive aircraft comprises a fuselage (1), a wing (2), fins (3), a landing gear (4), a main engine unit (5), an auxiliary engine unit (7), pylons (10) and external suspension objects (9). At least one suspension object (9) is arranged on the lower surface and the end of the wing (2). A gun unit or a guidance and tracking unit (8) is mounted in the lower part of the fuselage (1). The integrated control system of an airborne radioelectronic equipment (17) is provided with a power supply system (16) and a weapon control facility (19) which comprises, connected to each other and to the integrated control system of an airborne radioelectronic equipment (17) by means of a multiplex information exchange channel, the an airborne radioelectronic guidance and tracking system (20), a defence system (21), a multipurpose control board (22), a group interaction system (23) and a weapon control system (24). Said weapon control system (24) comprises a synchroniser and logic unit (25), an emergency unloading unit (26), an information distribution and conversion unit (27), actuators (28), an external suspension object switching unit (29) and a unit (30) for switching the suspended gun system or the suspended guidance and tracking system. The components of the weapon control system (24) are connected by means of a local information exchange channel. The number of the actuators (28) and the external suspension object switching units (29) corresponds to the number of the suspension objects (9).