CONVERTER FOR CONVERTING A LOAD FACTOR COMMAND INTO A LONGITUDINAL ATTITUDE DEVIATION INSTRUCTION

摘要

The invention relates to flight control systems for aircraft having large control loops delivering load factor commands and which are applied to flight controls more suited to the tracking by the pilot of a longitudinal attitude deviation instruction than to the tracking of a load factor instruction. It consists of a small control loop which generates a deviation indicator displayed by the flight director on the PFD screen with a converter for converting a load factor command into a longitudinal attitude deviation instruction (30) comprising a band-pass filter (305) allowing the integration for the calculation of the longitudinal attitude deviation instruction value in the piloting frequency range only.