METHOD FOR DISPLAYING AN ATTITUDE CONTROL INDICATOR IN A HEADS-UP DISPLAY SYSTEM FOR AN AIRCRAFT

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...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	SACHEAU, Romain, AYMERIC, Bruno, BARREAU, Jonathan
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	GYROSCOPIC INSTRUMENTS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION OPTICAL ELEMENTS, SYSTEMS, OR APPARATUS OPTICS PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS SURVEYING TESTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	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.