Asymmetric torque switching for aircraft autopilot

Details Asymmetric torque switching for aircraft autopilot Asymmetric torque switching for aircraft autopilot

G - Physics

05

D

341/80

G05D 1/06 (2006.01) G05D 1/00 (2006.01)

Patent

CA 1242509

ABSTRACT OF THE DISCLOSURE An apparatus for providing asymmetrical torque switching for an aircraft autopilot. The invention provides an increased amount of available pitch servo torque at high altitude. The direction of pitch of the aircraft is sensed. An increased amount of torque is provided for the pitch-up direction thereby providing more positive control of the aircraft.

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