Pitch control system

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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Details

244 84, 244 87, B64C 1312

Patent

active

039499588

ABSTRACT:
An improved system of pitch control for aircraft having a "flying tail"; i.e., a movable horizontal stabilizer with at least one movable elevator thereon. The human or automatic pilot input commands operate the elevators, and then the elevator response is used as part of the command to operate the stabilizer.

REFERENCES:
patent: 1574567 (1926-02-01), Flettner
patent: 2613891 (1952-10-01), Knight
patent: 3109614 (1963-11-01), Steidl
patent: 3207458 (1965-09-01), Kean
patent: 3409251 (1968-11-01), Lawson et al.

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