Flight management computer system for aircraft, has inputting and parametering unit to input and parameterize speed constraint to be followed in landing runway approaching phase until constraint end point is crossed by aircraft

摘要

The system has an inputting and parametering unit for inputting and parametering geographical elements and flight constraints associated to the elements for defining a framework of a route. A guiding unit produces set points and orders concerning the management of engine thrust and aerodynamic configuration of an aircraft to follow a three dimensional path and respect the constraints. The parametering unit inputs and parameterizes speed constraint to be followed in a landing runway approaching phase until a constraint end point marked on the path or route is crossed by the aircraft.