FIELD: aircrafts.
SUBSTANCE: invention relates to a method for generating control commands to a steering drive in a roll channel of a stabilization system of an axisymmetric aircraft. To generate control commands, the angles of attack in two longitudinal control channels (αу, αz) and control commands (δI, δII, δэ) are determined in three control channels, the angle of aerodynamic roll is calculated in the onboard equipment of the stabilization system in a certain way, and taking into account the angle of aerodynamic roll, four control commands to the steering gear of the aircraft (δ1, δ2, δ3, δ4) to deflect each aerodynamic rudder in a certain way and supply these commands to the steering gear.
EFFECT: improved stabilization of the aircraft by reducing the effect of aerodynamic cross-coupling and decreasing oscillations of the aircraft.
1 cl, 17 dwg
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Authors
Dates
2021-12-30—Published
2021-05-14—Filed