| 摘要 |
<p>A helicopter having an automatic flight control system including an inner, stability loop is rendered less sensitive to short-term, inadvertent pilot inputs by applying a washed-out derivative (36) of a stick position signal (32) to the inner stability loop in a sense to countermand the pilot action. Using a washed-out signal countermands only short term rapid stick motions, which may be induced by the pilot actively, but inadvertently, or inactively due to coupling between the pilot or the stick and motion of the fuselage, while permitting purposeful longterm stick positions to have the full, intended effect. </p> |
