Electronic flight control system for an aircraft capable of hovering
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United States of America Patent
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Mar 24, 2015
Grant Date -
Jun 21, 2012
app pub date -
Jun 10, 2010
filing date -
Jun 10, 2009
priority date (Note) -
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Abstract
An electronic flight control system for an aircraft capable of hovering and having at least one rotor. The flight control system is configured to operate in a manual flight control mode, in which the flight control system controls rotor speed in response to direct commands from the pilot; and in at least two automatic flight control modes corresponding to respective flight modes of the aircraft, and in which the flight control system controls rotor speed automatically on the basis of flight conditions. The flight control system is also configured to memorize, for each automatic flight control mode, a respective flight table relating different speed values of the rotor to different values of at least one flight quantity; and to automatically control rotor speed in the automatic flight control modes on the basis of the respective flight tables.
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