Aerospace Instrument-Making Annotation << Back Checking and Diagnosis of complex failures in gas-turbine engine control systems with use of recurrent neural network S.V. Gernakov The problem of complex failures diagnosis in hydromechanical accelerating unit of aviation engine is considered. The example and technique of gas-turbine engine accelerating condition checking and diagnosis with use of recurrent neural network is presented. Key words: recurrent neural networks, algorithms of training, metric distance. E-mail: zhvs@rb.ru