| 摘要 |
FIELD: aircraft engineering. ^ SUBSTANCE: proposed device comprises device (2) to define control magnitude corresponding to instruction amount selected by pilot with the help of control member (3), and device (5) to adjust effective control magnitude corresponding to said instruction amount actually applied to aircraft. It comprises also device (6) to automatically control aircraft, device (11) to computer auxiliary control magnitude approximating to effective adjusted magnitude, and device (16) to exercise control over control magnitude and to reveal deviation generated by pilot. ^ EFFECT: automatic control using adjustable effective magnitude and auxiliary control magnitude. ^ 11 cl, 2 dwg |
