An aircraft assembly, comprising: a reference component; a first component (106) and a first actuator (102), the first actuator arranged to move the first component relative to the reference component; a second component (108) and a second actuator (102), the second actuator (102) arranged to move the second component relative to the reference component; a position sensor (110) arranged to measure a position of the first component (106), and to output a position value, the sensor being capable of outputting a plurality of non-zero position values; and a controller (100) arranged to control the movement of the second component (108) by the second actuator (104) based at least partially on the position value output by the position sensor (110).
AIRCRAFT LANDING GEAR ASSEMBLY ACTUATION SYSTEM
AKTUATORSYSTEM FÜR FLUGZEUGFAHRWERKSEINHEIT
SYSTÈME D'ACTIONNEMENT D'ASSEMBLAGE DU TRAIN D'ATTERRISSAGE D'AÉRONEF
2022-08-24
Patent
Electronic Resource
English
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