Roll attitude inhibit of aircraft coordinated turn disengagement

Details Roll attitude inhibit of aircraft coordinated turn disengagement Roll attitude inhibit of aircraft coordinated turn disengagement

1981-03-30

1983-02-01

Smith, Jerry

Boots, shoes, and leggings

244 1713, 244179, G06F 1550, B64C 1100

Patent

active

043719392

ABSTRACT:
The engagement (83) of a flight director (82) that provides automatic steering by roll angle of an aircraft which includes an automatic yaw trim system (FIG. 2) that will automatically coordinate turns induced by the flight director establishes (155, 157, 138) a heading hold disengagement mode which is maintained even if the flight director becomes disengaged (160) until the aircraft roll attitude is indicated as being nearly level (163). Exemplary roll channel (FIG. 1) and yaw channel (FIG. 2 ) of an automatic flight control system which may incorporate the invention are disclosed.

REFERENCES:
patent: 3711042 (1973-01-01), Rempfer et al.
patent: 4003532 (1977-01-01), Adams, Sr. et al.
patent: 4067517 (1978-01-01), Barnum
patent: 4094479 (1978-06-01), Kennedy, Jr.
patent: 4206891 (1980-06-01), Perez et al.
patent: 4213584 (1980-07-01), Tefft et al.

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