Canard (aeronautics) flown, including the Ambrosini SS.4, Curtiss-Wright XP-55 Ascender and Kyūshū J7W1 "Shinden". These were attempts at using the canard configuration to give advantages in areas such as performance, armament disposition or pilot view, but no production aircraft were completed. The Shinden was ordered into production "off the drawing board" but hostilities ceased before any other than prototypes had flown. Just after the end of World War II in Europe in 1945, what may have been the first canard designed and flown in the Soviet Union appeared as a test aircraft, the lightweight Mikoyan-Gurevich MiG-8 "Utka" (Russian for "duck"). It was
Canard (aeronautics) and the main wing, leading to issues with stability and behaviour in the stall. This limits their applicability. The development of fly-by-wire and artificial stability towards the end of the century opened the way for computerized controls to begin turning these complex effects from stability concerns into maneuverability advantages. This approach produced a new generation of military canard designs. The Dassault Rafale multirole fighter first flew in 1986, followed by the Saab Gripen (first to enter service) in 1988, the Eurofighter Typhoon in 1994 and the Chinese Chengdu J-10 in 1998. A canard foreplane may be used for various reasons