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
2018-12-11
Patent
Electronic Resource
English
Factors Pertaining to Installation of Inverted, In-Line AIRCOOLED AIRCRAFT ENGINES
SAE Technical Papers | 1946
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