| CPC B64C 29/0025 (2013.01) [B64D 27/24 (2013.01); B60L 2200/10 (2013.01)] | 21 Claims |

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1. An electric aircraft having fixed pitch lift, the aircraft comprising:
a plurality of flight components, wherein the plurality of flight components further comprises:
at least a lift propulsor component, wherein the lift propulsor component comprises a plurality of blades configured at an angle of attack; and
a flight controller, wherein the flight controller is configured to:
calculate a flight element using an intermediate representation; and
transmit the flight element to the plurality of flight components.
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