Thrust vector control method to increase the trajectory automatic control accuracy of the aircraft when landin

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Authors: Mulin P. V., Berezuev A. V., Kushnir D. M.

Annotation: A new method of thrust vectoring integration into control system is proposed for synthesis of control systems for new generation of aircrafts. This method is based on concept of synthesis of two channel system with fast and slow subsystems and limited control possibilities. It is shown that the control system of aircraft with thrust vectoring is an effective tool to increase the trajectory automatic control accuracy of the aircraft when landing.

Keywords: thrust vector control, elevator, automatic control system, aircraft