Automatic flight control system having unified graphic mistrim i

Details Automatic flight control system having unified graphic mistrim i Automatic flight control system having unified graphic mistrim i

1992-09-17

1994-10-25

Huppert, Michael S.

Aeronautics and astronautics

Miscellaneous

340973, 340976, 340979, G01C 2300

Patent

active

053581997

ABSTRACT:
An improved flight control system with an enhanced unified graphic mistrim indicator where the flight control computer provides signals to a single mistrim indicator wherein the signals represent the status of the control surfaces of the aircraft and the mistrim indicator displays a single movable reference marker, which is caused to be translated vertically in the event of pitch mistrim, is caused to be rotated right or left in the case of roll mistrim conditions, is caused to be translated right or left in the case of yaw mistrim conditions or is caused to be moved in a combination of ways either translating vertically, horizontally or rotating in order to represent a combination of pitch, roll or yaw mistrim.

REFERENCES:
patent: 3521228 (1970-07-01), Congleton et al.
patent: 4326189 (1982-04-01), Crane
patent: 4563742 (1986-01-01), McElreath
patent: 4663627 (1987-05-01), Dennis
patent: 5212480 (1993-05-01), Ferro

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