Methods and systems of displaying weather data for a cockpit display system of an aircraft. The methods and systems include generating a display to include a first graphical map of real-time weather data from a weather radar. The display further includes a notification graphic associated with a portion of part of a displayed flight plan in which a significant weather condition exists. When the notification graphic is selected, the display includes the first graphical map of the real time weather data based on weather data from the weather radar and a second graphical map of significant weather conditions data derived from transmitted weather data.

A system for mid-fidelity simulation may include a memory configured to store data representing a flight scenario. The system may further include a display device configured to present a graphical user interface to a user, the graphical user interface including representations of a first set of control interfaces, the first set of control interfaces including one or more features that are common between multiple aircraft, the graphical user interface omitting one or more features of the first set of control interfaces that are not common between the multiple aircraft. The system may also include a processor configured to perform a simulation of the flight scenario while receiving user input and displaying user output via the representations of the first set of control interfaces.

A system for mid-fidelity simulation may include a memory configured to store data representing a flight scenario. The system may further include a display device configured to present a graphical user interface to a user, the graphical user interface including representations of a first set of control interfaces, the first set of control interfaces including one or more features that are common between multiple aircraft, the graphical user interface omitting one or more features of the first set of control interfaces that are not common between the multiple aircraft. The system may also include a processor configured to perform a simulation of the flight scenario while receiving user input and displaying user output via the representations of the first set of control interfaces.

A system and method for a mobile flight simulator of an electric aircraft is illustrated. The first simulator housing instrument is configured to house a plurality of first flight simulator components. The second simulator housing instrument is configured to house a plurality of second flight simulator components. The pilot control is configured to receive a pilot command and transmit the pilot command to a computing device. The computing device is configured to communicatively connect each first flight simulator component of the plurality of flight simulator components and each second flight simulator component of the plurality of flight simulator components, generate a mobile flight simulation as a function of the pilot command, the mobile flight simulation including an electric aircraft model, and update the electric aircraft model as a function of the pilot command, the mobile flight simulation and a feedback datum.

A system and method for a mobile flight simulator of an electric aircraft is illustrated. The first simulator housing instrument is configured to house a plurality of first flight simulator components. The second simulator housing instrument is configured to house a plurality of second flight simulator components. The pilot control is configured to receive a pilot command and transmit the pilot command to a computing device. The computing device is configured to communicatively connect each first flight simulator component of the plurality of flight simulator components and each second flight simulator component of the plurality of flight simulator components, generate a mobile flight simulation as a function of the pilot command, the mobile flight simulation including an electric aircraft model, and update the electric aircraft model as a function of the pilot command, the mobile flight simulation and a feedback datum.

A system and method for a mobile flight simulator of an electric aircraft is illustrated. The first simulator housing instrument is configured to house a plurality of first flight simulator components. The second simulator housing instrument is configured to house a plurality of second flight simulator components. The pilot control is configured to receive a pilot command and transmit the pilot command to a computing device. The computing device is configured to communicatively connect each first flight simulator component of the plurality of flight simulator components and each second flight simulator component of the plurality of flight simulator components, generate a mobile flight simulation as a function of the pilot command, the mobile flight simulation including an electric aircraft model, and update the electric aircraft model as a function of the pilot command, the mobile flight simulation and a feedback datum.

A system and method for a mobile flight simulator of an electric aircraft is illustrated. The first simulator housing instrument is configured to house a plurality of first flight simulator components. The second simulator housing instrument is configured to house a plurality of second flight simulator components. The pilot control is configured to receive a pilot command and transmit the pilot command to a computing device. The computing device is configured to communicatively connect each first flight simulator component of the plurality of flight simulator components and each second flight simulator component of the plurality of flight simulator components, generate a mobile flight simulation as a function of the pilot command, the mobile flight simulation including an electric aircraft model, and update the electric aircraft model as a function of the pilot command, the mobile flight simulation and a feedback datum.

A system and method for an electric aircraft coaching simulator is illustrated. The simulator includes a pilot control that is configured to generate a pilot command. The simulator includes a processor that is configured to receive optimized flight data, simulate a battery performance of an electric aircraft as a function of the received pilot command and generate an optimal flight recommendation based off the optimized flight data. The simulation model is configured to communicatively connect with the flight simulator to mimic a real flight situation. Optimized flight data from other pilots can be used to coach pilots how to fly with more energy efficiency.

A system and method for an electric aircraft coaching simulator is illustrated. The simulator includes a pilot control that is configured to generate a pilot command. The simulator includes a processor that is configured to receive optimized flight data, simulate a battery performance of an electric aircraft as a function of the received pilot command and generate an optimal flight recommendation based off the optimized flight data. The simulation model is configured to communicatively connect with the flight simulator to mimic a real flight situation. Optimized flight data from other pilots can be used to coach pilots how to fly with more energy efficiency.

A computer system including a memory in communication with a processor, the memory storing instructions that when executed by the processor cause the processor to maintain a virtual environment, manage a virtual asset within the virtual environment, map a geospatial position of a real vehicle into a position within the virtual environment representative of the geospatial position. determine a measurement between the position of the real vehicle in the virtual environment to the virtual asset and communicate content representative of the virtual asset to a mixed reality optical system configured for an operator of the real vehicle, wherein the content is presented at a time and position based, at least in part, on the measurement.