Integrated automatic control system of longitudinal motion of aircraft with engine thrust control, and elevator.

Аuthors

Rybnikov S. I.^*, Kurmakov D. V.^**, Gorbachev Y. V.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: kaf301@mai.ru
**e-mail: dvkurmakov@gmail.com

Abstract

Solve problem of simultaneous control of engine thrust and elevator at take-off mode. Variability of the balanced angle of attack has shown on this mode.

Keywords:

safety of flight, optimal control, aircrafts, thrust control, estimated aerodynamic

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