The invention relates to a method for managing the speed restrictions of a flight plan of an aircraft, the method comprising the following steps: - identifying a flight phase in progress, - determining a CAS speed profile, the speed profile establishing a behaviour of the aircraft relative to a speed setpoint, - determining a Mach speed profile, the Mach speed profile establishing a behaviour of the aircraft relative to a Mach setpoint, the Mach setpoint being a speed setpoint written as an equivalent Mach number, - determining a crossover altitude, the crossover altitude being an altitude for switching from the aircraft being automatically controlled according to the CAS speed profile to being automatically controlled according to the Mach speed profile, - determining an end of applicability criterion for the speed profile and for the Mach speed profile.
PROCEDE DE CONSTRUCTION ET D'ASSERVISSEMENT D'UN PROFIL DE VITESSE COMPRENANT DES CONTRAINTES DE VITESSE AT OU AT OR ABOVE
METHOD FOR CONSTRUCTING AND AUTOMATICALLY CONTROLLING A SPEED PROFILE COMPRISING AT OR AT OR ABOVE SPEED RESTRICTIONS
VERFAHREN ZUR ERSTELLUNG UND AUTOMATISCHEN STEUERUNG EINES GESCHWINDIGKEITSPROFILS MIT BESCHRÄNKUNGEN FÜR DIE GESCHWINDIGKEIT BEI ODER ÜBER
2024-05-29
Patent
Elektronische Ressource
Französisch
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