In some embodiments, a pilot guidance display system may include a display operatively coupled to an aircraft and configured to provide a plurality of indications and a plurality of limits to a pilot. The pilot guidance display may also include a computing device operatively coupled to the aircraft and communicatively coupled to the display. The computing device may have at least one processor configured to update the plurality of indications and the plurality of limits on the display in real-time based at least in part on a plurality of conditions provided by a plurality of sensors on the aircraft. The plurality of limits may include a first maximum angle of attack indicator. Methods and computer implemented operations are also disclosed.
SYSTEM AND METHOD FOR A PILOT GUIDANCE DISPLAY OF AN AIRCRAFT
15.08.2024
Patent
Elektronische Ressource
Englisch
IPC: | G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS |
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