Manned aircraft

摘要

The aircraft (1) has a bearing surface (2) for producing lifting of the aircraft, and a lifting system (3) arranged behind the bearing surface in a flight direction for stabilizing flight position and controlling the aircraft. The lifting system is adjusted based on a parameter e.g. aerodynamically active surface area (Fh), elongation, sweeping angle (phih), wingspan (bh) and length of a lever arm of the lifting system. The parameter is adjusted depending on an operating parameter e.g. flight speed, of the aircraft. An independent claim is also included for a method for adjusting a parameter of a lifting system.