Adaptive flight display radio tuning system

An aircraft system, comprising:

• at least one civil radio implemented in an aircraft;
• at least one mission radio implemented in the aircraft;
• a display implemented in the aircraft;
• and
• an avionics computing device implemented in the aircraft, the avionics computing device comprising at least one processor and memory communicatively coupled to the at least one processor, the avionics computing device communicatively coupled to the at least one civil radio, the at least one mission radio, and the display, the memory configured to maintain at least one civil radio tuning system application and at least one mission radio tuning system application, each of the at least one civil radio tuning system application being associated with a particular civil radio of the at least one civil radio, each of the at least one mission radio tuning system application being associated with a particular mission radio of the at least one mission radio, the at least one processor configured to:
• execute the at least one civil radio tuning system application and the at least one mission radio tuning system application;
• tune the at least one civil radio and the at least one mission radio;
• generate a graphical user interface multifunction window comprising a plurality of slots, each slot being assignable to display information associated with one of the at least one civil radio tuning system application and the at least one mission radio tuning system application;
• assign each of at least one first particular slot of the plurality of slots to display information associated with the at least one civil radio tuning system application;
• assign each of at least one second particular slot of the plurality of slots to display information associated with the at least one mission radio tuning system application;
• and
• output, to the display, the graphical user interface multifunction window having particular slots filled with the information associated with the at least one civil radio tuning system application and the at least one mission radio tuning system application;
• wherein the display is configured to present, to a user, the graphical user interface multifunction window having the particular slots filled with the information associated with the at least one civil radio tuning system application and the at least one mission radio tuning system application.

A method of operating an aircraft system, comprising:

• executing, by at least one processor of an adaptive flight display implemented in an aircraft, at least one civil radio tuning system application and at least one mission radio tuning system application, the adaptive flight display comprising a display, the at least one processor, and memory communicatively coupled to the at least one processor, the adaptive flight display communicatively coupled to at least one civil radio and at least one mission radio implemented in the aircraft, the memory configured to maintain the at least one civil radio tuning system application and the at least one mission radio tuning system application, each of the at least one civil radio tuning system application being associated with a particular civil radio of the at least one civil radio, each of the at least one mission radio tuning system application being associated with a particular mission radio of the at least one mission radio;
• tuning, by the at least one processor, the at least one civil radio and the at least one mission radio;
• generating, by the at least one processor, a graphical user interface multifunction window comprising a plurality of slots, each slot being assignable to display information associated with one of the at least one civil radio tuning system application and the at least one mission radio tuning system application;
• assigning, by the at least one processor, each of at least one first particular slot of the plurality of slots to display information associated with the at least one civil radio tuning system application;
• assigning, by the at least one processor, each of at least one second particular slot of the plurality of slots to display information associated with the at least one mission radio tuning system application;
• outputting, by the at least one processor, to the display, the graphical user interface multifunction window having particular slots filled with the information associated with the at least one civil radio tuning system application and the at least one mission radio tuning system application;
• and
• presenting, by the display of the adaptive flight display, to a user, the graphical user interface multifunction window having the particular slots filled with the information associated with the at least one civil radio tuning system application and the at least one mission radio tuning system application.