| 摘要 |
<p>An aircraft having servo mechanisms for adjusting the flying control surfaces in accordance with movement of the flying control lever 12 by the pilot. A feedback system controlled by a computer monitors the variation in power transmitted through the servo mechanism for a flying control surface during an aerobatic manoeuvre initiated by the control surface, and applies to the flying control lever 12 a feedback force which is representative of the variation in power. The computer is programmed so that port and starboard actuators (15,16 and 13,14, fig 2) exert increasing tactile force on the control lever in accordance with aircraft speed.</p> |
