Design of Robust Aircraft Control System

The paper is devoted to approaches designing aircraft control systems based on the robust approach. Such a research of great importance for operated in conditions accompanied by perturbations. structural synthesis chosen as main tool problem solving. mathematical descriptions both deterministic and stochastic are considered. Dryden filter models represented. state-space approach used. H-infinity synthesis, function mixed sensitivity, loop-shaping given. Features Robust Control Toolbox necessary automated studied. weight transfer functions augmentation plant model proposed. result simulation system shown transient processes lateral longitudinal motions. proposed directed providing possibility operate influence possible applications obtained results controls motion civil aviation.