A feedback system controlled by a computer monitors the variation in power transmitted through the servo mechanism (13, fig 2),15,(20),22 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 tactile force is relatively weak when the aerobatic manoeuvre is performed at a speed close to stalling speed and is relatively strong when the aerobatic manoeuvre is performed at a speed close to the maximum permissible speed at cruising altitudes.
Improvements in aircraft
2015-07-08
Patent
Electronic Resource
English
Online Contents | 2005
|IEEE | 2005
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