An exemplary method for controlling low speed flight of an aircraft having a controller receiving pilot input includes transitioning from a translational rate command, TRC, (302) to a linear acceleration command, LAC, (310) when the controller is displaced above a control transition displacement, CTD, (304) and while in LAC (310) holding speed when the controller is relaxed to CTD (304).
HYBRID LOW SPEED CONTROL
HYBRIDE NIEDERGESCHWINDIGKEITSSTEUERUNG
COMMANDE HYBRIDE À FAIBLE VITESSE
2024-05-01
Patent
Elektronische Ressource
Englisch