METHOD AND SYSTEM FOR CONTROLLING THE VARIABLE-PITCH VANES OF A GUIDE OF A LOW-PRESSURE COMPRESSOR OF AN AIRCRAFT TURBINE ENGINE

摘要

The invention relates to a method for controlling the variable-pitch vanes of a guide (121) of a low-pressure compressor (120) of an aircraft turbine engine (100) on the basis of a plurality of pre-obtained parameters relating to said low-pressure compressor and to a high-pressure compressor (130) located downstream of the low-pressure compressor along a drive shaft. The invention also relates to a control system (1) for implementing said control method.