Apparatus and methods for a fuel-based flight indicator apparatus for an electric aircraft
A fuel-based flight indicator apparatus for an electric aircraft is illustrated. The apparatus comprises a flight indicator and a computing device communicatively connected to the flight indicator, wherein the computing device is configured to receive a battery datum from a battery sensor located in the electric aircraft, receive an environmental datum from an environmental sensor located in the electric aircraft, determine an indicator datum as a function of the battery datum, the environmental datum, and a flight plan, and display the indicator datum on the flight indicator.
1. A fuel-based flight indicator apparatus for an electric aircraft, the fuel-based flight indicator apparatus comprising:
a flight indicator;
a computing device communicatively connected to the flight indicator, wherein the computing device comprises a processor and a memory containing instructions configuring the processor to:
receive a battery datum from a battery sensor located in the electric aircraft;
receive an environmental datum from an environmental sensor located in the electric aircraft;
determine an indicator datum as a function of the battery datum, the environmental datum, and a flight plan, wherein determining the indicator datum comprises:
calculating an estimated usable energy of an energy source of the electric aircraft as a function of the battery datum; and
comparing the estimated usable energy and the environmental datum to the flight plan,
wherein the indicator datum includes an indication of a probability of success of the flight plan; and
display the indicator datum on the flight indicator.
2. The fuel-based flight indicator apparatus of claim 1 , wherein the electric aircraft is configured to perform vertical take-off and landing.
3. The fuel-based flight indicator apparatus of claim 1 , wherein the electric aircraft is configured to perform short takeoff and landing.
4. The fuel-based flight indicator apparatus of claim 1 , wherein determining the indicator datum further comprises determining the indicator datum as a function of a flight variable.
5. The fuel-based flight indicator apparatus of claim 4 , wherein the flight variable comprises information related to a battery degradation of the energy source.
6. The fuel-based flight indicator apparatus of claim 1 , wherein determining the indicator datum further comprises use of a look up table to perform an array indexing operation to replace a runtime computation of the processor.
7. The fuel-based flight indicator apparatus of claim 1 , wherein the battery datum is detected by the battery sensor as a function of a battery phenomenon.
8. The fuel-based flight indicator apparatus of claim 1 , wherein the indicator datum represents whether or not fuel remaining in a battery is sufficient enough to complete the flight plan.
9. The fuel-based flight indicator apparatus of claim 1 , wherein the indicator datum further comprises a score indicating the probability of completion of the flight plan, wherein the score is generated as a function of a defuzzied probability of success.
10. The fuel-based flight indicator apparatus of claim 1 , wherein the environmental datum comprises information related to weather conditions surrounding the electric aircraft.
11. A method for a fuel-based flight indicator apparatus for an electric aircraft, the method comprising:
communicatively connecting a computing device to a flight indicator;
receiving, at the computing device, a battery datum from a battery sensor located in the electric aircraft;
receiving, at the computing device, an environmental datum from an environmental sensor located in the electric aircraft;
determining, at the computing device, an indicator datum as a function of the battery datum, the environmental datum, and a flight plan, wherein determining the indicator datum comprises:
calculating an estimated usable energy of an energy source of the electric aircraft as the function of the battery datum; and
comparing the estimated usable energy and the environmental datum the flight plan,
wherein the indicator datum includes an indication of a probability of probability of success of the flight plan; and
displaying, at the computing device, the indicator datum on the flight indicator.
12. The method of claim 11 , wherein the electric aircraft is configured to perform vertical take-off and landing.
13. The method of claim 11 , wherein the electric aircraft is configured to perform short takeoff and landing.
14. The method of claim 11 , wherein determining the indicator datum further comprises determining the indicator datum as a function of a flight variable.
15. The method of claim 14 , wherein the flight variable comprises information related to a battery degradation of the energy source.
16. The method of claim 11 , wherein determining the indicator datum further comprises use of a look up table to perform an array indexing operation to replace a runtime computation of the computing device.
17. The method of claim 11 , wherein the battery datum is detected by the battery sensor as a function of a battery phenomenon.
18. The method of claim 11 , wherein the indicator datum represents whether or not fuel remaining in a battery is sufficient enough to complete the flight plan.
19. The method of claim 11 , wherein the indicator data further comprises a score indicating the probability of completion of the flight plan, wherein the score is generated as a function of a defuzzied probability of success.
20. The method of claim 11 , wherein the environmental datum comprises information related to weather conditions surrounding the electric aircraft.