Method and apparatus for aircraft pitch and thrust axes control
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United States of America Patent
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-
Sep 11, 1984
Issued Date -
N/A
app pub date -
Oct 28, 1983
filing date -
Sep 20, 1982
priority date (Note) -
Expired
status (Latency Note)
Importance
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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