FIELD: aircraft engineering.
SUBSTANCE: this invention allows the drone to get to preset point in preset time and to combine several drones into rank at target attack section. Device for implementation of proposed methods comprises the object of control, engine, first module of calculation, first, second and third module of switching, first, second, third and fourth addition modules, first and second integration modules, amplification module, transmission factor calculation module, control signal limitation module, current fuel consumption determination module, current available fuel rate calculation module and control signal generation module.
EFFECT: decreased weight and overall dimensions, accelerated data processing, higher validity of results used for fuel flow rate control.
3 cl, 1 dwg
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