Systems and methods for determining remaining useful energy in an electric aircraft
A system for determining remaining useful energy in an electric aircraft, the system including a computing device where the computing device is configured to measure a internal state datum of a battery as a function of at least a sensor, receive the internal state datum from the at least a sensor, generate a useful energy remaining datum as a function of the internal state datum and a battery model, and display the useful energy remaining datum to a user.
1. A system for determining remaining useful energy in an electric aircraft, the system comprising a computing device, wherein the computing device is configured to:
measure an internal state datum of a battery on an electric aircraft as a function of at least a sensor, wherein the at least a sensor comprises at least a gas sensor;
receive the internal state datum from the at least a sensor;
train a battery model using training data, wherein the training data includes battery internal state datum correlated to battery remaining useful energy data;
generate a useful energy remaining datum as a function of the internal state datum and the battery model;
calculate a remaining flight range based on a flight plan and the useful energy remaining datum;
display a hologram of a depth of discharge of the battery based on the useful energy remaining datum; and
display, a calculated thermal runaway prediction of the electric aircraft.
2. The system of claim 1 , wherein the training data is updated at preset intervals.
3. The system of claim 1 , wherein the training data is stored in a database on the electric aircraft.
4. The system of claim 1 , wherein the computing device is further configured to generate a battery degradation rate as a function of the internal state datum and the battery model.
5. The system of claim 4 , wherein the computing device is further configured to display the battery degradation rate to the user.
6. The system of claim 1 , wherein the computing device is further configured to generate a thermal datum as a function of the internal state datum and the battery model.
7. The system of claim 6 , wherein the computing device is configured to calculate a probability of a thermal runaway as a function of the thermal datum.
8. The system of claim 7 , wherein the computing device is further configured to display a warning to the user as a function of the calculation.
9. The system of claim 1 , wherein the computing device is further configured to display the remaining flight range as a function of the useful energy remaining datum.
10. A method for determining remaining useful energy in an electric aircraft, the method comprising:
measuring, by a computing device, an internal state datum of a battery on an electric aircraft as a function of at least a sensor, wherein the at least a sensor comprises at least a gas sensor;
receiving, by the computing device, the internal state datum from the at least a sensor;
training, by the computing device, a battery model using training data, wherein the training data includes battery internal state datum correlated to battery remaining useful energy data; and
generating, by the computing device, a useful energy remaining datum as a function of the internal state datum and the battery model;
calculating, by the computing device, a remaining flight range based on a flight plan and the useful energy remaining datum;
displaying, by the computing device, a hologram of a depth of discharge of the battery based on the useful energy remaining datum; and
displaying, by the computing device, a calculated thermal runaway prediction of the electric aircraft.
11. The system of claim 10 , wherein the training data is updated at preset intervals.
12. The method of claim 10 , wherein the training data is stored in a database on the electric aircraft.
13. The method of claim 10 , wherein the method further comprises generating, by the computing device, a battery degradation rate as a function of the internal state datum and the battery model.
14. The method of claim 13 , wherein the method further comprises displaying, by the computing device, the battery degradation rate to the user.
15. The method of claim 10 , wherein the method further comprises generating, by the computing device, a thermal datum as a function of the internal state datum and the battery model.
16. The method of claim 15 , wherein the method further comprises calculating, by the computing device, a probability of a thermal runaway as a function of the thermal datum.
17. The method of claim 16 , wherein the method further comprises displaying, by the computing device, a warning to the user as a function of the calculation.
18. The method of claim 10 , wherein the method further comprises displaying, by the computing device, the remaining flight range as a function of the useful energy remaining datum.
19. The system of claim 9 , wherein the computing device is further configured to display the remaining flight range as a function of the useful energy remaining datum and a flight plan.
20. The method of claim 18 , wherein the method further comprises displaying, by the computing device, the remaining flight range as a function of the useful energy remaining datum and a flight plan.