Method and apparatus for producing an aircraft flare path control signal
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United States of America Patent
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-
Oct 12, 1982
Grant Date -
N/A
app pub date -
Jun 24, 1980
filing date -
Jun 24, 1980
priority date (Note) -
Expired
status (Latency Note)
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Abstract
Aircraft altitude, ground velocity, and altitude rate signals are input to a computer which, using a unique control law, generates a pitch control surface command signal suitable for guiding an aircraft on its flare path to a specified runway touchdown point despite varying wind conditions.
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