Electronic throttle control system for aircraft

摘要

An electronic control apparatus comprising: a movable control member (12); a positional servo loop means including at least one motor means (22,24) and being operable to maintain the position of said control member at any one of a plurality of positions in the range of movement thereof in accordance with a demand signal; force detection means (48) for detecting a force applied to said control member and for providing to said servo loop means a demand signal which varies in accordance with the magnitude of said applied force. <IMAGE>