HYBRIDSYSTEM ZUR STEUERUNG EINES FLUGZEUGMOTORS UND VERFAHREN ZUR STEUERUNG DAVON

摘要

The system for controlling a proposed aircraft engine comprises: - at least one feedback loop, - at least one state feedback control integrated in the feedback loop. The state feedback control comprises a static compensator (M) and a state corrector loop (L) which are configured so as to decouple the states formed by the operating parameters of the engine to be controlled. The monovariable controllers are then configured in such a way that the operating parameters are controlled by the commands.