Robust integrated flight and propulsion control (IFPC) of an experimental STOVL aircraft

The technique of /spl Hscr//sup /spl infin// loop-shaping is used to design a robust integrated flight and propulsion controller for an experimental STOVL aircraft configuration, based on the Harrier T.Mk 10 airframe with a Rolls Royce Spey engine. Performance properties of the integrated controller are validated via nonlinear simulation.