Aircraft in-flight center of gravity measuring system

Details Aircraft in-flight center of gravity measuring system Aircraft in-flight center of gravity measuring system

G - Physics

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354/16

G06G 7/70 (2006.01) G01M 1/12 (2006.01)

Patent

CA 1211567

Abstract of the Disclosure In order to determine the location of the center of gravity of an aircraft in flight, an accel- erometer is placed in the forward part of the aircraft and another is placed in the after part to produce signals representing the rotation of aircraft about an axis, preferrably the yaw axis, through the aircraft center of gravity. The signals from the acceler- ometers are combined to produce a first signal having components that represent both motion of the aircraft and the location of the center of gravity along with a signal having a component representing the motion of the aircraft but substantially without a component representing the location of the center of gravity and these two signals are then combined to yet a signal that represents the location of the aircraft center of gravity.

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