An aircraft avionic system for use in an equipped aircraft includes a controller and a display. The controller provides output data to the display, with the output data producing visual images on the display. An angle of attack data source provides current angle of attack data for the equipped aircraft. The controller is responsive to the angle of attack data in order to provide the output data to drive the display to depict a direction of control needed to preclude a stall. The display of direction of control needed is graduated based on a current level of stall imminence. The stall imminence is a function of the angle of attack of the equipped aircraft.
INTUITIVE DISPLAY OF ANGLE OF ATTACK GUIDANCE ON AIRCRAFT ATTITUDE INDICATOR
AFFICHAGE INTUITIF DE GUIDAGE D'ANGLE D'ATTAQUE SUR UN INDICATEUR D'ASSIETTE D'AERONEF
2018-01-04
Patent
Electronic Resource
English
INTUITIVE DISPLAY OF ANGLE OF ATTACK GUIDANCE ON AIRCRAFT ATTITUDE INDICATOR
European Patent Office | 2018
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