Rotorcraft fly-by-wire control laws
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United States of America Patent
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-
Jul 26, 2016
Issued Date -
N/A
app pub date -
Dec 19, 2014
filing date -
Apr 1, 2014
priority date (Note) -
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status (Latency Note)
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Abstract
According to one embodiment, a flight control system includes a pilot control module configured to receive commands from a pilot, a flight control module operable to transmit an instruction to change at least one operating condition of an aircraft, and a flight control computer in communication between the flight control module and the pilot control module. The flight control computer is configured to receive a pilot command to change a first flight characteristic, wherein changing the first flight characteristic would result in an expected change to a second flight characteristic. The flight control computer may instruct the flight control module to transmit an instruction to change a first operating condition of the aircraft and instruct the flight control module to transmit an instruction to change a second operating condition of the aircraft to at least partially offset the expected change to the second flight characteristic.
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