Systems and methods for remote pilot control of an electric aircraft
A system for remote pilot control of an electric aircraft in autopilot mode including a remote computing device configured to receive a user input and generate a control datum as a function of the pilot input, a flight controller configured to receive the control datum from the remote computing device, and generate a command datum as a function of the control datum and an authority status, and the remote computing device configured to receive the command datum from the flight controller, and display the command datum.
1. A system for remote pilot control of an electric aircraft during autopilot, the system comprising:
a flight controller communicatively connected to a remote computing device and an electric aircraft, wherein the flight controller is configured to:
receive a control datum from a remote computing device, wherein the remote computing device is communicatively connected to a pilot control;
determine an authority status of the control datum, wherein the authority status comprises a level of control from a plurality of levels of control, that a user has over the electric aircraft, wherein the plurality of levels of control comprises a full level of control and a partial level of control;
generate a command datum as a function of the control datum and the authority status; and
initiate an operation of a flight component of the electric aircraft as a function of the command datum and the authority status.
2. The system of claim 1 , wherein the full level of control comprises full authority over the electric aircraft.
3. The system of claim 1 , wherein the pilot control is located remotely from the electric aircraft.
4. The system of claim 1 , wherein the flight controller is further configured to transmit the command datum to the remote computing device.
5. The system of claim 1 , wherein initiating an operation of the flight component of the electric aircraft comprises commanding at least an actuator to actuate the flight component as a function of the command datum.
6. The system of claim 1 , wherein the flight controller is further configured to transmit the authority status to the remote computing device.
7. The system of claim 1 , wherein generating the command datum, when authority status comprises the partial level of control, comprises:
generating a flight control algorithm; and
generating the command datum as a function of the command datum and the authority status.
8. The system of claim 1 , wherein the flight controller comprises a plurality of flight controllers.
9. The system of claim 8 , wherein the plurality of flight controllers comprises a first flight controller in a first location and a second flight controller in a second location.
10. The system of claim 1 , wherein the control datum indicates a pilot's desire to change a heading of the electric aircraft.
11. A method for remote pilot control of an electric aircraft during autopilot, the method comprising:
receiving, by a flight controller of an electric aircraft, a control datum from a remote computing device, wherein the remote computing device is communicatively connected to a pilot control;
determining, by the flight controller, an authority status of the control datum, wherein the authority status comprises a level of control from a plurality of levels of control, that a user has over the electric aircraft, wherein the plurality of levels of control comprises a full level of control and a partial level of control;
generating, by the flight controller, a command datum as a function of the control datum and the authority status; and
initiating, by the flight controller, an operation of a flight component of the electric aircraft as a function of the command datum and the authority status.
12. The method of claim 11 , wherein the full level of control comprises full authority over the electric aircraft.
13. The method of claim 11 , wherein the pilot control is located remotely from the electric aircraft.
14. The method of claim 11 , further comprising transmitting, by the flight controller, the command datum to the remote computing device.
15. The method of claim 11 , wherein initiating an operation of the flight component of the electric aircraft comprises commanding at least an actuator to actuate the flight component as a function of the command datum.
16. The method of claim 11 , further comprising transmitting, by the flight controller, the authority status to the remote computing device.
17. The method of claim 11 , further comprising generating, by the flight controller, the command datum, when authority status comprises the partial level of control, comprising:
generating a flight control algorithm; and
generating the command datum as a function of the command datum and the authority status.
18. The method of claim 11 , wherein the flight controller comprises a plurality of flight controllers.
19. The method of claim 18 , wherein the plurality of flight controllers comprises a first flight controller in a first location and a second flight controller in a second location.
20. The method of claim 11 , wherein the control datum indicates a pilot's desire to change heading of the electric aircraft.