Systems and methods for a heads-up display for an electric aircraft
A system for a head-up display for an electric aircraft is presented. The system includes an augmented reality device which may be operated by a pilot using a pilot device and a computing device connected to the pilot device, wherein the computing device is configured to receive an aircraft datum and generate a performance assessment model. The performance assessment model includes a plurality of information relevant to the operation of the electric aircraft. The augmented reality device further includes a projection device configured to project the performance assessment model onto an exterior view window and display the performance assessment model as a function of the projection device.
1. An electric aircraft having a head-up display, the electric aircraft comprising:
at least a propulsor configured to generate thrust using an electric motor;
at least a battery configured to power the electric motor of the at least a propulsor;
a pilot device located within a physical cockpit and configured for use by a pilot;
a computing device comprising at least a microprocessor communicatively connected to the pilot device, wherein the computing device is configured to:
receive an aircraft datum; and
generate a performance assessment model as a function of the aircraft datum, wherein the performance assessment model comprises at least a flight phase model depicting the power consumption of at least a battery for at least a portion of the flight
an exterior view window configured to allow viewing of the surroundings of the electric aircraft and
a data display component configured to display the performance assessment model on the exterior view window, wherein the data display comprises a plurality of projection devices arranged in a concave formation.
2. The electric aircraft of claim 1 , wherein the pilot device further comprises a sensor, wherein the sensor is configured to:
detect measured aircraft data, including a battery system datum associated with the at least a battery; and
generate the aircraft datum as a function of the measured aircraft data.
3. The electric aircraft of claim 1 , wherein the electric aircraft comprises an electric vertical take-off and landing aircraft wherein, the at least a propulsor comprises a lift propulsor configured to generate lift and a thrust propulsor configured to generate forward thrust.
4. The electric aircraft of claim 1 , wherein the exterior view window is further configured to display a live feed.
5. The electric aircraft of claim 4 , wherein the computing device is further configured to adjust the displaying of the performance assessment model based on the live feed.
6. The electric aircraft of claim 1 , wherein the data display component includes at least a projection device.
7. The electric aircraft of claim 6 , wherein the at least a projection device further comprises a first projection device configured to project a first display datum and a second projection device configured to project a second display datum, wherein the first display datum is distinct from the second display datum.
8. The electric aircraft of claim 1 , wherein the pilot device further comprises a multifunction display.
9. The electric aircraft of claim 1 , wherein the pilot device further comprises a primary flight display.
10. The electric aircraft of claim 1 , wherein the pilot device is further configured to control which information is to be displayed onto the exterior view window.
11. A method for an electric aircraft having a head-up display, the method comprising:
generating, using at least a propulsor, thrust using an electric motor;
powering, using at least a battery, the electric motor of the at least a propulsor;
receiving, by a computing device comprising at least a microprocessor communicatively connected to a pilot device located within a physical cockpit and configured for use by a pilot, an aircraft datum;
generating a performance assessment model as a function of the aircraft datum, wherein the performance assessment model comprises at least a flight phase model depicting the power consumption of at least a battery for at least a portion of the flight; and
displaying, by a data display component, the performance assessment model onto an exterior view window configured to allow viewing of the surroundings of the electric aircraft, wherein the data display comprises a plurality of projection devices arranged in a concave formation.
12. The method of claim 11 , wherein the method further comprises:
detecting, by a sensor communicatively connected to the pilot device, measured aircraft data, including a battery system datum associated with the at least a battery; and
generating the aircraft datum as a function of the measured aircraft data.
13. The method of claim 11 , wherein the electric aircraft comprises an electric vertical take-off and landing aircraft, wherein the at least a propulsor comprises a lift propulsor configured to generate lift and a thrust propulsor configured to generate forward thrust.
14. The method of claim 11 , wherein the method further comprises displaying, by the exterior view window, a live feed.
15. The method of claim 14 , wherein displaying the live feed further comprises adjusting the displaying of the performance assessment model based on the live feed.
16. The method of claim 11 , wherein the data display component includes at least a projection device.
17. The method of claim 16 , wherein the method further comprises:
displaying, by a first projection device, a first display datum; and
displaying, by a second projection device, a second display datum, wherein the second display datum is distinct from the first display datum.
18. The method of claim 11 , wherein the pilot device further comprises a multifunction display.
19. The method of claim 11 , wherein the pilot device further comprises a primary flight display.
20. The method of claim 11 , wherein the method further comprises controlling, by the pilot device, which information is to be displayed onto the exterior view window.