Systems and methods for determining areas of discrepancy in flight for an electric aircraft
A system for determining areas of discrepancy in flight for an electric aircraft is presented. The system includes a plurality of sensors, wherein each sensor is communicatively connected to a flight component and configured to detect a measured flight and generate a flight phase datum. The system further includes a computing device communicatively connected to the plurality of sensors, wherein the computing device is configured to determine, by a flight phase machine-learning model, a flight phase discrepancy datum. The computing device is configured to train the flight phase machine-learning using a flight phase training set, wherein the flight phase training set correlates a flight phase to a flight standard and output the flight phase discrepancy datum. The computing device is further configured to identify an anomalous performance phase as a function of the flight phase discrepancy datum and generate a discrepancy response.
1. A system for determining areas of discrepancy in flight for an electric aircraft, the system comprising:
a plurality of sensors, wherein each sensor is communicatively connected to a flight component of an electric aircraft and configured to:
detect a measured flight datum; and
generate a flight phase datum as a function of the measured flight datum; and
a computing device communicatively connected to the plurality of sensors, the computing device configured to:
determine, using a flight phase machine-learning model and the flight phase datum, a flight phase discrepancy datum;
identify an anomalous performance phase as a function of the flight phase discrepancy datum; and
generate an anomaly response as a function of an anomalous source wherein the anomalous source is identified as a function of a comparison of the flight phase discrepancy datum and a flight phase history datum retrieved from an aircraft datum database and the anomaly response comprises:
at least a maintenance report; and
at least a corrective action, wherein the at least a corrective action comprises:
an aerodynamic drag induction, the aerodynamic drag induction comprising recuperating aerodynamic energy; and
at least a strike force command.
2. The system of claim 1 , wherein the plurality of sensors comprises:
a first sensor configured to detect a first measured flight datum of the flight component at a first time interval; and
a second sensor configured to detect a second measured flight datum of the flight component at a second time interval.
3. The system of claim 2 , wherein the computing device is further configured to determine the flight phase discrepancy datum as a function of the first measured flight datum and the second measured flight datum.
4. The system of claim 1 , wherein the sensor is further configured to generate a flight component datum as a function of the measured flight datum.
5. The system of claim 4 , wherein the computing device is further configured to:
determine a flight component discrepancy datum as a function of the flight component datum;
identify an anomalous performance flight component as a function of the flight component discrepancy datum; and
generate the anomaly response as a function of the anomalous performance flight component.
6. The system of claim 1 , wherein the computing device is further configured to generate the anomaly response during flight.
7. A method for determining areas of discrepancy in flight for an electric aircraft, the method comprising:
detecting, by a sensor communicatively connected to a flight component of an electric aircraft, a measured flight datum;
generating a flight phase datum as a function of the measured flight datum;
determining, by a computing device communicatively connected to the sensor, a flight phase discrepancy datum;
identifying an anomalous performance phase as a function of the flight phase discrepancy datum; and
generating an anomaly response as a function of an anomalous source wherein the anomalous source is identified as a function of a comparison of the flight phase discrepancy datum and a flight phase history datum retrieved from an aircraft datum database and the anomaly response comprises:
at least a maintenance report; and
at least a corrective action, wherein the at least a corrective action comprises:
an aerodynamic drag induction, the aerodynamic drag induction comprising recuperating aerodynamic energy; and
at least a strike force command.
8. The method of claim 7 , wherein the method further comprises:
detecting, by a first sensor communicatively connected to the flight component, a first measured flight datum at a first time interval; and
detecting, by a second sensor communicatively connected to the flight component, a second measured flight datum at a second time interval.
9. The method of claim 8 , wherein the method further comprises determining the discrepancy datum as a function of the first measured flight datum and the second measured flight datum.
10. The method of claim 7 , wherein the method further comprises generating a flight component datum as a function of the measured flight datum.
11. The method of claim 10 , wherein the method further comprises:
determining, by the computing device, a flight component discrepancy datum as a function of the flight component datum;
identifying an anomalous performance flight component as a function of the flight component discrepancy datum; and
generating the anomaly response as a function of the anomalous performance flight component.
12. The method of claim 7 , wherein the method further comprises generating the anomaly response during flight.