FIELD: aircraft controlling methods.
SUBSTANCE: invention relates to a method for controlling an aircraft in the ACS "go-around" mode. To control the aircraft, the indicated airspeed is formed taking into account the maximum allowable flight speed (VFE) for the current position of the flaps and slats with linear interpolation between the nodal points, taking into account the speed reduction margin determined by the range protection function (RPF) of the speed parameters in a certain way. When the ACS "go-around" mode is turned on, the autothrottle is turned on, in the thrust channel, the stabilization mode of the indicated airspeed set on the ACS control panel, corresponding to the flight with the wing mechanization removed, is immediately switched on, while the autothrottle, depending on the flight conditions, controls the engine control levers ( thruster) so that, together with trajectory control in the longitudinal channel, to provide the desired climb with normalized climb gradients and acceleration to mechanization harvesting speeds.
EFFECT: automation of the control process in the "go-around" mode and increase in flight safety is provided.
1 cl, 7 dwg, 1 tbl
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Authors
Dates
2023-03-28—Published
2022-04-06—Filed