History of Science and Engineering Annotation << Back AIRCRAFT SPEED AUTOMATIC CONTROL CONSEPT DEVELOPMENT A.V. Grebenkin, A.Z. Akhromeyev, D.U. Gladkaya The generation of a complex control impact on an aircraft engine thrust and drag component for fl ight speed management based on the logic of multilevel adaptation to flight conditions according to fuel effi ciency, engine life and given fl ight speed stabilization accuracy criteria concept development is considered in this article. It covers the complex approach to flight speed management in a historical perspective Keywords: multilevel adaptation; primary and secondary control signal; engine thrust. Contacts: E-mail: aomiea@aviapribor.ru Pp. 036-049.