Roll attitude inhibit of aircraft automatic outer loop

Details Roll attitude inhibit of aircraft automatic outer loop Roll attitude inhibit of aircraft automatic outer loop

1981-03-30

1983-06-07

Smith, Jerry

Boots, shoes, and leggings

244 1713, 244177, G06F 1550, G06G 778

Patent

active

043874312

ABSTRACT:
In an aircraft automatic flight control system (FIG. 4) the application of force to a control member (35R, FIG. 5) forces (222, 216, 217, 212, 213) the flight path controlling, full authority outer loop to be disengaged. Once disengaged by force, the outer loop remains disengaged (224) until force is removed (225) and a signal indicates (226) a need to reestablish the outer loop. Reestablishment may be indicated by beeping (228) or by the controlled attitude (54R, 55R) being restored to within a predetermined level (230).

REFERENCES:
patent: 4004756 (1977-01-01), Gerstine et al.
patent: 4029271 (1977-06-01), Murphy et al.
patent: 4078750 (1978-03-01), Tomlinson
patent: 4109886 (1978-08-01), Tribken et al.
patent: 4213584 (1980-07-01), Tefft et al.
patent: 4279391 (1981-07-01), Adams et al.

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