FIELD: engines and pumps.
SUBSTANCE: control of gas-turbine engine (GTE) with afterburner is performed as per one of three control loops; individual control programme is specified on each loop and corrected as per certain group of sensors the readings of which are the most essential for operation exactly in that mode.
EFFECT: invention allows improving operating reliability and safety of GTE with afterburner of airborne vehicle due to reducing the time of augmented and full acceleration of GTE and expansion of safe startup area of afterburner, and providing GTE operation in wide range in optimum modes.
2 cl, 1 dwg
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