Automatic pitch axis control system for aircraft

Details Automatic pitch axis control system for aircraft Automatic pitch axis control system for aircraft

1974-01-18

1977-02-08

Kunin, Stephen G.

Aeronautics and astronautics

Aircraft control

Automatic

23515022, G05D 112

Patent

active

040068714

ABSTRACT:
An aircraft flight control system utilizing inertial sensor input signals for providing glide slope and flare control signals in the aircraft. The autopilot approach and landing coupler system is a vertical velocity command control system utilizing signals representative of integrated vertical acceleration for providing feedback signals representative of vertical velocity and utilizing signals representative of ground velocity to provide the switchless glide slope and flare vertical velocity command signals.

REFERENCES:
patent: 3223362 (1965-12-01), Doniger
patent: 3295796 (1967-01-01), Gaylor
patent: 3327973 (1967-06-01), Kramer et al.
patent: 3447765 (1969-06-01), Doniger et al.
patent: 3652835 (1972-03-01), Devlin et al.
patent: 3743221 (1973-07-01), Lykken et al.

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