| CPC B64C 13/18 (2013.01) [G05D 1/0858 (2013.01); G05D 1/102 (2013.01)] | 17 Claims |
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1. A system for hybrid autonomous control of an electric aircraft, the system comprising:
at least one sensor, wherein the at least one sensor is configured to:
detect a first aircraft position datum;
detect a first aircraft rate datum;
detect a throttle position of a throttle control for an electric propulsion unit; and
transmit the first aircraft position datum, the first aircraft rate datum, and the throttle position to a flight controller;
a flight controller, wherein the flight controller is configured to:
receive the first aircraft position datum;
receive the first aircraft rate datum;
receive the throttle position; and
generate a recommended autopilot output based on the throttle position, the first aircraft position datum, the first aircraft rate datum, and at least one of a target value or a threshold value; and
a display located within the electric aircraft, wherein the display is configured to:
receive the recommended autopilot output from the flight controller; and
display the recommended autopilot output.
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