LANDING GEAR CONTROLLER

Abstract: a landing gear controller that: determines whether a predetermined criterion is met; and causes a power supply system of an aircraft to supply power to an actuation system of the aircraft to cause a component of a landing gear system of the aircraft to move from a first position to a second position selectively according to: a first predetermined supplied-power profile, when the landing gear controller determines that the predetermined criterion is not met, and a second predetermined supplied-power profile, according to which a maximum power supplied by the power supply system to the actuation system is greater than a maximum power supplied by the power supply system to the actuation system according to the first predetermined supplied-power profile, to move the component from the first position to the second position more quickly, when the landing gear controller determines that the predetermined criterion is met.

Inventor(s): Sean KERR, Mark JOHNSON

CPC Classification: B64C25/26 (Control or locking systems therefor)

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