Analytical design of the automatic control system of the roll angle of the medium-haul aircraft with an elastic wing according to the variable criterion

Nguyen Thanh Son, Ribnhikov Sergey Igorevich

The analytic design of the automatic control system of the automatic control system with the angle of roll of the medium-haul aircraft taking into account the flexural nonrigidity of the wing is carried out, according to the variable criterion, the change in the parameter leads to a counter change in the speed of the system and energy consumption for control while maintaining the high quality of the transient processes.

Keywords:Analytical design, energy consumption, roll angle control, aeroelastic wing movements.