FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft control methods and hardware. In compliance with proposed method, to reduce vertical turbulence effects, wind vertical component and danger level are automatically determined. Aids for automatic computation of control instructions are used to minimise load factor variation amplitude caused by vertical turbulence. Proposed device comprises moving element to act on aircraft lift, aids to determine wind vertical component and danger level, those to compute and transmit control instructions and to check up activation conditions.
EFFECT: possibility to reduce vertical turbulence effects.
18 cl, 2 dwg
