Abstract
The use of modern computer technology in the development of new aircraft contributes to the improvement of their characteristics in terms of flight safety due to more advanced information processing algorithms that ensure the identification of dangerous (emergency) aircraft motion modes. The detected violations in the operation of the equipment make it possible to change the algorithm for generating control actions on board. In order to identify a failure, it is proposed to use a correlation algorithm, for the implementation of which an algorithm has been developed for generating databases according to the quantitative characteristics of the development of failures in the form of Z-transfer functions. The redesign of the control algorithm is carried out in the form of implementing the Euler—Lagrange optimality conditions, where the control function iteration method is used.
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