| 摘要 |
The flight control device (1) comprises, in addition to a control member (2) and to a means of actuation of a controlled member (RP, RQ), a means of determination (MD) for determining a control command which corresponds to a translational rate control command, dependent on the deflection of the control member (2), while the translational rate of the aircraft (He) is less than a reference value and which corresponds otherwise to a translational acceleration or angular rate control command, dependent on an extra deflection of the control member (2).
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