MULTI-FUNCTIONAL MISSION GRIP SYSTEM FOR A VEHICLE

摘要

The present invention relates to a mission grip system (1) which enables the pilot/copilot to control the critical mission equipment in aircrafts simultaneously, and basically comprises a pilot mission grip (2); a copilot left hand mission grip (3) and/or a copilot right hand mission grip (4); at least one gun interface unit (10), which is adapted to generate control signals according to the discrete control and condition signals coming from the mission grips for controlling and firing the gun units in the aircraft and to transmit these signals to the gun unit that will be controlled; a weapon interface unit (11) which is adapted to generate the power and discrete signals required to fire the missiles integrated to the aircraft; a mission computer (12) which is adapted to control all mission equipment such as moving digital map system, weapon system and target detection/sighting system of the aircraft and to provide the data transmission between the said equipment; at least one control unit (15) which is adapted to generate the power signals required for the mission grips, and to collect the parallel data coming from the mission grips and to transmit the said data serially to the mission computer (12).