System and method for automated flight correction in an electric aircraft
AssigneeBeta Air, LLC
InventorHerman Wiegman
Life of this patent
Estimating the term…
Abstract
A system for automated flight correction in an electric aircraft includes an input control configured to generate a control datum, at least a sensor connected to the electric aircraft, wherein the at least a sensor is configured to detect a status datum, and a flight controller communicatively connected to the input control and the at least a sensor, wherein the flight controller is configured to determine a command datum as a function of the control datum and the status datum, wherein determining the command datum comprises comparing the control datum to a limitation set based on the status datum, and calculating a modified control datum based on a flight plan of the electric aircraft through a remote device.
Claims20
A system for automated flight correction in an electric aircraft, the system comprising:
- an input control configured to generate a control datum;
- a sensor connected to the electric aircraft, wherein the sensor is configured to detect a status datum;
- and
- a flight controller communicatively connected to the input control and the sensor, wherein the flight controller is configured to:
- determine a command datum as a function of the control datum and the status datum, wherein determining the command datum comprises:
- comparing the control datum to a limitation set based on the status datum;
- and
- calculating a modified control datum based on a flight plan of the electric aircraft through a remote device.
A method for automated flight correction in an electric aircraft, the method comprising:
- generating, at an input control, a control datum;
- detecting, at a sensor, a status datum;
- and
- determining, at a flight controller, a command datum as a function of the control datum and the status datum, wherein determining a command datum comprises:
- comparing the control datum to a limitation set based on the status datum;
- and calculating a modified control datum based on a flight plan of the electric aircraft through a remote device.
Dependencies are inferred from the claim text.