Method and apparatus for aircraft pitch and thrust axes control

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244181, 244182, G05D 108

Patent

active

043576630

ABSTRACT:
An aircraft automatic or 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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