Aircraft coordinated turn with lagged roll rate

Details Aircraft coordinated turn with lagged roll rate Aircraft coordinated turn with lagged roll rate

1981-03-30

1983-07-05

Smith, Jerry

Boots, shoes, and leggings

244 1713, 244177, G06F 1550, G06G 778

Patent

active

043922031

ABSTRACT:
An aircraft automatic flight control system having a roll channel (FIG. 1), a yaw outer loop trim system (bottom of FIG. 2) and a yaw stability inner loop (top of FIG. 2) provides proportional (129) and integral (114) lateral acceleration inputs to the yaw trim system (106, 93) during coordinated turns, and provides proportional (130) and lagged (131) roll rate inputs to the trim system to provide initial coordination to the turns.

REFERENCES:
patent: 3711042 (1973-01-01), Rempfer et al.
patent: 3812333 (1974-05-01), Mineck et al.
patent: 3848833 (1974-11-01), Rauschelbach
patent: 4067517 (1978-01-01), Barnum
patent: 4109886 (1978-08-01), Tribken et al.
patent: 4206891 (1980-06-01), Perez et al.

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