Method for determining the center of gravity for an aircraft and system for determining the center of gravity for an aircraft

摘要

Method for determining the center of gravity for an aircraft and system for determining the center of gravity for aircraft systems and methods for determining the center of gravity for an aircraft.An example system includes one or more load measuring devices that generate information about the weight of the landing gear nose or main landing gear and a processing device which determines the center of gravity of the aircraft based on the information of the gross weight before Iormente received and the information generated from the weight of the landing gear nose or at the landing gear principaL. the number of sets of landing gear with load measuring devices is one less than the total number of sets of landing gear having distinct longitudinal positions along the length of a fuselage of the aircraft. The processing device additionally determines the center of gravity based on the temperature and / or information of the attitude of the longitudinal tilt.The system includes a user interface that allows a user to enter with the information of the gross weight that can be included in a manifesto of vu00f3o or umaplanilha load and compensation and / or a communication component that receives the information of the gross weight from a base system ADO in the earth.