A new flight control design scheme using optimal dynamic output feedback

Thispaper applies anewly developed optimal dYnami output feedback control methodtocontrol thea of attack a andpitch angle 0(for longtudinal control), andtheangle ofsideslip 3androll angle 4(for lateraldirectional control), sothatpilot canmeuverandcontrol theairplane tothedesired flight attitude prec... View More