Heading reference trim system

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Details

244178, 318585, 318586, B64C 1308

Patent

active

046269983

ABSTRACT:
A heading trim reference system provides beep commands indicative of a desired heading/attitude change to the roll channel of an AFCS as roll commands at slow speed in a conventional manner, and to the yaw channel as yaw commands at cruise speed. At cruise speed, the yaw synchronizing integrator responds to the beep commands and provides an error signal to existing turn coordination logic to turn the aircraft.

REFERENCES:
patent: 3711042 (1973-01-01), Rempfer et al.
patent: 3848172 (1974-11-01), Thomas
patent: 4003532 (1977-01-01), Adams et al.
patent: 4067517 (1978-01-01), Barnum
patent: 4213584 (1980-07-01), Tefft et al.
patent: 4330829 (1982-05-01), Fischer et al.

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