Complemented roll attitude flight control system

Details Complemented roll attitude flight control system Complemented roll attitude flight control system

1982-08-17

1985-11-12

Krass, Errol A.

Boots, shoes, and leggings

318585, 244179, G06F 1530

Patent

active

045532109

ABSTRACT:
A system and technique is disclosed which provides a complemented roll attitude signal for use in the control system of an aircraft. The complemented roll attitude is produced by combining a yaw rate and true airspeed signal with a conventional roll attitude signal to produce a complemented signal which may be combined with a roll command signal to produce a roll steering signal for controlling aircraft response under non-zero roll attitude conditions of aircraft flight. The complemented roll attitude signal provides improved response to aircraft roll commands under non-zero roll attitude conditions, particularly in helicopter systems.

REFERENCES:
patent: 3057584 (1962-10-01), Bretoi
patent: 3147424 (1964-09-01), Miller
patent: 3417945 (1968-12-01), Reynolds et al.
patent: 3901466 (1975-08-01), Lambregts
patent: 4148452 (1979-04-01), Niessen et al.
patent: 4198017 (1980-04-01), Murray
patent: 4330829 (1982-05-01), Fischer et al.
patent: 4343035 (1982-08-01), Tanner
patent: 4371939 (1983-02-01), Adams et al.

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