Process and device for automatically determining a recapture route from a flight path for an aircraft, so as system and method for automatically guiding an aircraft

摘要

The method involves forming a capture trajectory (TC) in three phases in which initial phase (PH1) represents a rotation of an aircraft (A) in an arc of circle (6). The transition phase (PH2) has a rectilinear segment (7) having a capture angle with respect to a rectilinear section (2) of a flight line (TO). The end phase (PH3) represents a rotation permitting the aircraft to rejoin with the section. The Independent claims are also included for the following: (A) a method for guiding an aircraft (B) an aircraft comprising a system for guiding the aircraft and a device for determining a capture trajectory of a flight line of an aircraft.