METHOD FOR DETERMINING CONDITIONS OF POSSIBLE UNMANNED AIRCRAFT LAUNCH Russian patent published in 2017 - IPC G06G7/80 F41G7/00 G05D1/00 

FIELD: aviation.

SUBSTANCE: for determining the launch possibilities target coordinates, number and position of rout change points, gunnery course, approach to the target angle, target designation angle, target characteristic and size, fuel type, wind speed are entered using the first user interface, current parameters of the carrier are displayed, expected target search root point, unmanned aircraft (UMAC) time of reaching the attack line, probability of target capture by active radar-homing head, minimum and maximum range of the UMAC use, method of detecting target, the total UMAC flight path to the target, required amount of fuel are calculated at regular intervals in the calculating module and displayed on the screen of the second carrier user interface, UMAC flight path diagram, the tatget, rout change points,UMAC flight path, target position ambiguity area, target search root point, attack line radius, antenna roll angle are displayed on the screen using the third user interface, flight mission is transmitted to the UMAC and start enabling signal is made if parameters enter specified limiting range.

EFFECT: accuracy of determining the UMAC launch command moment from different types of carriers.

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