Rolling airframe autopilot

Details Rolling airframe autopilot Rolling airframe autopilot

G - Physics

05

D

341/80

G05D 1/08 (2006.01) G05D 1/10 (2006.01)

Patent

CA 1087714

ROLLING AIRFRAME AUTOPILOT ABSTRACT OF THE DISCLOSURE The autopilot incorporates a single linear accelerometer transducer and a single pitch rate sensor. the outputs of the accelerometer and pitch rate sensor are summed with the command signal in the control circuit. A servo is controlled by the modified control signal to vary the incidence of a single plane control system, in an intentionally rolling airframe.

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