CPC B64D 45/00 (2013.01) [B64C 29/0016 (2013.01); G05D 1/102 (2013.01); G06N 20/00 (2019.01); G07C 5/085 (2013.01); B64D 2045/0085 (2013.01); G05D 1/0038 (2013.01)] | 20 Claims |
1. A system for data verification of an electric aircraft at start up, the system comprising:
at least an electrical component;
a health monitoring system comprising a sensor, wherein the sensor is configured to detect an operational datum from the at least an electric component;
a flight controller communicatively connected to the at least an electrical component, the flight controller configured to:
start the electric aircraft;
receive an operational datum from the health monitoring system;
identify a software datum of each software system of a plurality of software systems of the electric aircraft;
perform a data verification, wherein the data verification comprises using a machine-learning process configured to:
receive the operational datum and the software datum as inputs; and
determine an assessment datum and a software status datum as a function of the inputs, wherein the software status datum includes a comparison of the software datum to an acceptance criterion; and
generate an output datum from the assessment datum and the software status datum; and
an output device, wherein the output device comprises a heads-up display (HUD) disposed in a pilot headwear, the output device configured to:
display the output datum.
|