Method and apparatus for aircraft pitch and thrust axes control

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244181, 244182, 340978, G05D 108

Patent

active

044714394

ABSTRACT:
An aircraft automatic of semiautomatic vertical path control system which coordinates operation of pitch and engine thrust control systems to transfer speed control from one system to the other depending on a requirement to climb, descend, or maintain altitude as determined by the polarity and magnitude of the difference between a selectable desired altitude and current actual altitude.

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patent: 4237540 (1980-12-01), Sato
patent: 4277041 (1981-07-01), Marrs et al.
patent: 4312041 (1982-01-01), DeJonge

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