CPC B64C 13/503 (2013.01) [B64C 13/0421 (2018.01); G05D 1/0077 (2013.01)] | 20 Claims |
1. A system for fly-by-wire reversionary flight control, the system comprising:
an electric aircraft, wherein the electric aircraft is configured to include:
a first control element;
a first actuator coupled to the first control element, wherein the first actuator is configured to:
receive a control data;
determine a first command datum as a function of the control data and a distributed control algorithm; and
actuate a first control element as a function of the first command datum.
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