Acceleration limited preselect altitude capture and control

Aeronautics and astronautics – Aircraft control – Automatic

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Details

364433, 364434, 318584, G05D 108

Patent

active

041148428

ABSTRACT:
The altitude acquisition and control system cooperates in an aircraft flight controller for permitting a previously selected altitude to be quickly captured without excessive acceleration of the craft normal to the flight path, even though the human pilot may have neglected to arm the automatic capture mode of the apparatus until after the time that the automatic capture mode is normally commanded.

REFERENCES:
patent: 3167276 (1965-01-01), Moosbrugger et al.
patent: 3240446 (1966-03-01), Miller
patent: 3510092 (1970-05-01), Hendrick et al.
patent: 3524612 (1970-08-01), Ainsworth et al.
patent: 3892373 (1975-07-01), Doniger

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