QFT for the Design of an Aircraft Flight Control
Abstract
Aircraft flight control has a multivariable and non linear nature that makes itsuitable for a verification of control capability of different designs. QFT techniques havebeen thoroughly used during the last years to provide robust control designs while usingclassic theory of control. The QFT method is applied to the design of an aircraft flightcontrol and the results, evaluated by means of an automated software, can be compared toresults obtained with different methodology approaches.
