In the method according to the invention, when the head support is oriented in a determined direction making, with the horizon line and/or with the “speed vector”, an angle greater than a first value, and/or when at least one of the attitude parameters of the aircraft becomes greater than a second value, the attitude director indicator is displayed locally in a reference frame tied to the head support and in the field of the viewing device.
METHOD OF DISPLAYING AN "ATTITUDE DIRECTOR INDICATOR" IN A HEAD VIEWING SYSTEM FOR AIRCRAFT
2017-06-15
Patent
Electronic Resource
English
INTUITIVE DISPLAY OF ANGLE OF ATTACK GUIDANCE ON AIRCRAFT ATTITUDE INDICATOR
European Patent Office | 2018
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