A computer-implemented flight display system including a computer processor that is capable of determining a current energy situation of an aircraft, an electronic display device, and a graphical user interface (GUI) provided on the electronic display device. The GUI includes a current aircraft position symbol, an optimal aircraft position symbol, and at least one symbol indicating a position for changing aircraft configuration. Relative positioning on the GUI of the optimal aircraft position system and the at least one symbol indicating a position for changing aircraft configuration is based at least in part on the determined current energy situation of the aircraft.
AIRCRAFT DISPLAY SYSTEM PERTAINING TO ENERGY MANAGEMENT
DIE ENERGIEVERWALTUNG BETREFFENDES FLUGZEUGANZEIGESYSTEM
SYSTÈME D'AFFICHAGE D'AÉRONEF SE RAPPORTANT À LA GESTION D'ÉNERGIE
2021-04-14
Patent
Elektronische Ressource
Englisch
AIRCRAFT DISPLAY SYSTEM PERTAINING TO ENERGY MANAGEMENT
Europäisches Patentamt | 2017
|Aircraft display system pertaining to energy management
Europäisches Patentamt | 2018
|Factors pertaining to installation of inverted, in-line aircooled aircraft engines
Engineering Index Backfile | 1946
|Measurements Pertaining to Air-Sea Interaction With a Small Instrumented Aircraft
British Library Conference Proceedings | 2000
|Factors Pertaining to Installation of Inverted, In-Line AIRCOOLED AIRCRAFT ENGINES
SAE Technical Papers | 1946
|