FIELD: aircraft engineering.
SUBSTANCE: invention relates to automated control systems and aircraft start control systems. Model is based on simulation statistical modelling method, comprises a unit of functional tasks of the computer system (CS), a unit for setting/reception of the solution parameters, a unit for setting/reception of the investigated object (IO) parameters and the environment parameters, a unit for simulating the control objects (CO) coming to the point of association with the IO, an IO distribution unit, a unit for calculating performance indicators of the CO start.
EFFECT: technical result is expansion of functional capabilities of the model, higher efficiency of the aircraft use.
1 cl, 2 dwg
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