| CPC B64C 13/503 (2013.01) [B60L 3/12 (2013.01); B60L 2200/10 (2013.01); H04L 2012/40215 (2013.01)] | 21 Claims |

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1. A system, comprising:
a flight component of an electric aircraft;
a plurality of inverters configured to energize the flight component by delivering AC power thereto, and communicatively coupled to one another; and
a plurality of flight controllers communicatively connected to the plurality of inverters via a plurality of communication buses, wherein a first flight controller of the plurality of flight controllers is directly connected to a first inverter of the plurality of inverters via a first communication bus and indirectly connected to a second inverter of the plurality of inverters via the first communication bus and the first inverter, the first flight controller lacking a connection to the second inverter via a communication bus, the plurality of flight controllers configured to:
receive an input;
generate a command as a function of the input; and
transmit the command to the plurality of inverters.
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