Asymmetric torque switching for aircraft autopilot

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

1985-08-15

1987-01-20

Shoop, Jr., William M.

Electricity: motive power systems

Positional servo systems

Vehicular guidance systems with single axis control

318565, 244180, 244181, B64C 1318

Patent

active

046382291

ABSTRACT:
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.

REFERENCES:
patent: 3934222 (1976-01-01), Bateman et al.
patent: 4032094 (1977-06-01), Morgan et al.
patent: 4281811 (1981-08-01), Nixon

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