LANDING ARRANGEMENT FOR REDUCING A DISTANCE ERROR OF A LANDING AIRCRAFT HAVING A HIGH LIFT-TO-DRAG RATIO

摘要

A landing arrangement for reducing a distance error of a landing aircraft having a high lift-to-drag ratio is disclosed. The landing arrangement comprises a longitudinal landing device (200, 230) having a surface adapted to allow gliding or rolling of the aircraft thereon, and a sloping device (240, 250) configured to set an angle of the longitudinal landing device (200, 230) with respect to a horizontal plane.