CPC G05D 1/101 (2013.01) [B64D 15/12 (2013.01); G01C 21/20 (2013.01); B64C 29/0008 (2013.01)] | 20 Claims |
1. An apparatus for pre-flight preparation for an electric aircraft, comprising:
at least one processor; and
a memory communicatively connected to the at least one processor, the memory containing instructions configuring the at least one processor to:
generate aircraft conditioning data associated with the electric aircraft using at least one sensor, wherein the aircraft conditioning data comprises:
a humidity datum comprising a specific humidity within the electric aircraft and a dew point within a cabin of the electric aircraft,
a temperature within the electric aircraft, and
a temperature external to the electric aircraft; and
activate an aircraft conditioning system using power from an auxiliary power supply independent from a main power supply of the electric aircraft, wherein the aircraft conditioning system comprises a wing defrosting system having heating coils embedded within at least one wing of the electric aircraft, and wherein the aircraft conditioning system is configured to:
generate heat using the heating coils as a function of the temperature external to the electric aircraft, and
control a humidity level within the cabin of the electric aircraft through temperature regulating elements and as a function of the humidity datum and the temperature within the electric aircraft.
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