| 摘要 |
One embodiment of the present invention is a method for automatically red ucing the effect of a component of an external force that is laterally incid ent on a rotorcraft. A signal of the rotorcraft indicative of and proportion al to the component is monitored. An absolute value of the signal and a pres et high limit are compared. If the absolute value is greater than the preset high limit, manual heading control of the rotorcraft is disabled and the he ading of the rotorcraft is adjusted with respect to the external force so as to decrease the lateral component of the external force experienced by the rotorcraft.
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