Werner, HerbertHerbertWernerMeister, TiloTiloMeister2023-02-012023-02-011999-04-30Control Engineering Practice 7 (3): 305-313 (1999)http://hdl.handle.net/11420/14709A new multimodel approach to robust controller design is illustrated by a practical application: for a laboratory aircraft model, a robust controller is designed for acceptable performance, in normal operating conditions and under propeller failure, simultaneously. Based on a linear model for each operating mode, linear matrix inequality (LMI) formulation of the problem and convex programming are used to search for a state feedback controller that achieves the objective. This state feedback design is then realized simultaneously in both operating modes by a controller that is based on fast output sampling. Robust performance is demonstrated by experimental results.en0967-0661Control engineering practice19993305313Elsevier ScienceLinear matrix inequalitiesMeasurement noiseMultirateOutput feedbackRobust controlSampled-data controlState feedbackTrade-offsTechnikIngenieurwissenschaftenRobust control of a laboratory aircraft model via fast output samplingJournal Article10.1016/S0967-0661(98)00190-7Journal Article