| 摘要 |
FIELD: aircraft control units. ^ SUBSTANCE: proposed device includes correcting unit for limitation of control signal at lead; magnitude of lead is calculated in correcting unit on principle of transfer function. Proposed method consists in introduction of limitation at lead on control signal of elevator control system till moment of attaining maximum angle of attack; magnitude of lead is calculated on principle of transfer function. ^ EFFECT: enhanced safety of aircraft maneuvering. ^ 3 cl, 10 dwg, 2 tbl |
