FIELD: aeronautical engineering. SUBSTANCE: control of fuel flow in proportion to deviation of current acceleration from desired value provides for maintenance of desired characteristic in respect to turbocompressor rotor acceleration. Propeller blade control proportional to deviation of current propeller acceleration from desired value provides for maintenance of desired characteristic in respect to propeller acceleration. Desired acceleration value of propeller is formed in proportion to desired tuning of propeller frequency of rotation in respect to desired rotor acceleration and in inverse proportion to desired tuning of rotor frequency of rotation. EFFECT: improved agreement between regulation programs for gas generator and propeller fan during transients. 4 dwg
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