Adaptive decentralized control of maneuver airplanes for large attack angles

摘要

The possibility of using adaptation methods for the solution of the problem of special isolated forms of motion that correspond to separate control of phase coordinates of a flying vehicle is discussed. This can sig- nificantly improve the maneuverability properties of the vehicle. A structure of an adaptive system for control of lateral motion of an airplane is obtained. This structure realizes the autonomy of channels of roll and yaw as well as decentralization by inputs and prescribed quality of isolated forms of motion.