Aircraft weight and balance system with automatic loading error correction

摘要: A weight and balance system which automatically compensates for loading errors while the aircraft is stationary. signal generated from outputs of a pair inclinometers mounted on adjacent opposite ends landing gear member bends in response to weight. The just after no movement detected held latch. subsequently are combined provide representative difference therebetween. scaled by an error correction coefficient compensation with corrected signal. further includes means performing reasonableness tests restoration power has been down. include determining whether had moved or there load change during If determined have occurred, latch reset hold restored. down