System for electric aircraft navigation
AssigneeBeta Air, LLC
InventorCollin Freiheit
Life of this patent
Estimating the term…
Abstract
A system for electric aircraft navigation includes a sensor configured to detect a navigation signal, a flight controller, wherein the flight controller is configured to receive the navigation signal, identify a navigation status as a function of the navigation signal, and determine an aircraft adjustment as a function of the navigation status, and a pilot display, wherein the pilot display is configured to display the aircraft adjustment to a user, and present an autonomous function configured to enact the aircraft adjustment automatically.
Claims20
A system for electric aircraft navigation, the system comprising:
- a sensor configured to detect a navigation signal;
- a flight controller, wherein the flight controller is configured to:
- receive the navigation signal;
- determine an aircraft adjustment as a function of the navigation signal;
- and
- generate an autonomous function configured to enact the aircraft adjustment in part by controlling at least a propulsor of an electric aircraft, wherein the at least a propulsor is electrically powered;
- and
- a pilot display located within the electric aircraft, wherein the pilot display is configured to:
- display the aircraft adjustment to a user.
A method of electric aircraft navigation, the method comprising:
- detecting, using a sensor, a navigation signal;
- receiving, using a flight controller, the navigation signal;
- determining, using the flight controller, an aircraft adjustment as a function of the navigation signal;
- generating, using the flight controller, an autonomous function configured to enact the aircraft adjustment in part by controlling at least a propulsor of an electric aircraft, wherein the at least a propulsor is electrically powered;
- and
- displaying, using a pilot display located within the electric aircraft, the aircraft adjustment to a user.
Dependencies are inferred from the claim text.