High speed turn coordination for rotary wing aircraft

Details High speed turn coordination for rotary wing aircraft High speed turn coordination for rotary wing aircraft

1991-08-28

1993-08-24

Peters, Jr., Joseph F.

Aeronautics and astronautics

Aircraft, heavier-than-air

Helicopter or auto-rotating wing sustained, i.e., gyroplanes

364434, G06F 1550

Patent

active

052382036

ABSTRACT:
A helicopter flight control system (21) includes a model following control system architecture which automatically provides a coordinating yaw command signal to the helicopter tail rotor to coordinate helicopter flight during a banked turn. The control system processes information from a variety of helicopter sensors (31) in order to provide the coordinating yaw command signal on an output line (72) to the tail rotor (20) of the helicopter.

REFERENCES:
patent: 3057584 (1962-10-01), Bretoi
patent: 3688099 (1972-08-01), Buscher
patent: 4003532 (1977-01-01), Adams et al.
patent: 4067517 (1978-01-01), Barnum
patent: 4106094 (1978-08-01), Land
patent: 4206891 (1980-06-01), Perez et al.
patent: 4312039 (1982-01-01), Skutecki
patent: 4313201 (1982-01-01), Fischer et al.
patent: 4371939 (1983-02-01), Adams et al.
patent: 4382283 (1983-05-01), Clelford et al.
patent: 4477876 (1984-10-01), Wright et al.
patent: 4484283 (1984-11-01), Verzella et al.
patent: 4626998 (1986-12-01), Adams et al.

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