MIXED SYSTEM FOR AVIATION ENGINE CONTROL AND CORRESPONDING REGULATION METHOD Russian patent published in 2022 - IPC G05B11/32 B64C13/16 

FIELD: computer technology.

SUBSTANCE: present technical solution relates to the field of computer technology for aviation. A system for aviation engine control contains a tracking contour, which receives set values of engine operating parameters at an input, and which controls the system together with a feedback contour according to these operating parameters. In this case, the tracking contour contains a decentralized control unit with one-dimensional regulators, a control unit with status feedback, embedded in the tracking contour. The specified control unit receives output data of the decentralized control unit with one-dimensional regulators at an input, and it is a feedback contour between engine operating parameters and outputs of the specified decentralized control unit, while the feedback contour issues engine control parameters. In this case, the control unit with status feedback is made with the possibility of decoupling of the specified operating parameters, while one-dimensional regulators of the decentralized control unit are made with the possibility of automatic regulation of the specified operating parameters according to set values of these parameters.

EFFECT: provision of full decoupling with simultaneous preservation of a possibility of simple corrector regulation.

12 cl, 7 dwg