Systems and methods for controlling a flight boundary of an aircraft
A system for controlling a flight boundary of an aircraft. The system includes a flight controller communicatively connected to the aircraft. The flight controller is configured to receive a plurality of flight data linked with the aircraft, determine a flight boundary for the aircraft as a function of the plurality of flight data, set an aircraft movement limit as a function of the flight boundary, receive a thrust envelope, and generate a control signal for the aircraft as a function of the aircraft movement limit and the thrust envelope. The control signal is limits the aircraft to remain within the flight boundary. A method for controlling a flight boundary of an aircraft is also provided.
1. A system for controlling a flight boundary of an aircraft, the system comprising:
a pilot control configured to interface with a pilot and transmit a thrust envelope;
a flight controller, wherein the flight controller is communicatively connected to the pilot control and an aircraft, wherein the flight controller is configured to:
receive a plurality of flight data linked with the aircraft, wherein a flight datum of the plurality of flight data comprises a flight component datum informing on an operation of a flight component, wherein the flight component comprises a propulsor component;
determine a flight boundary for the aircraft as a function of the plurality of flight data;
set an aircraft movement limit as a function of the flight boundary, wherein setting an aircraft movement limit comprises receiving an instruction, wherein the instruction includes an aircraft identifier and a specified value of the aircraft movement limit;
receive the thrust envelope, wherein the thrust envelope comprises an instruction to set a thrust envelope parameter; and
generate a control signal for the aircraft as a function of the aircraft movement limit and the thrust envelope, wherein the control signal limits the aircraft to remain within the flight boundary; and
an electric propulsor communicatively connected to the flight controller and configured to:
receive the control signal; and
control operation as a function of the control signal.
2. The system of claim 1 , wherein the flight boundary defines a three dimensional space for a flight trajectory of the aircraft.
3. The system of claim 1 , wherein determining the flight boundary for the aircraft further comprises:
training a machine-learning process with training data correlating aircraft flight data and aircraft flight boundary data; and
generating the flight boundary for the aircraft as a function of the machine-learning process.
4. The system of claim 1 , wherein the plurality of flight data comprises a weather datum.
5. The system of claim 1 , wherein the plurality of flight data comprises a location datum.
6. The system of claim 1 , wherein the plurality of flight data comprises a flight component datum.
7. The system of claim 1 , wherein the plurality of flight data comprises an energy capacity datum.
8. The system of claim 1 , wherein the plurality of flight data comprises an aircraft identity datum.
9. The system of claim 1 , wherein the aircraft comprises an electric aircraft.
10. The system of claim 1 , wherein the aircraft comprises an electric vertical takeoff and landing (eVTOL) aircraft.
11. A method for controlling a flight boundary of an aircraft, the method comprising:
interfacing, by a pilot control, with a pilot;
transmitting, by the pilot control, a thrust envelope;
receiving, by a flight controller communicatively connected to the pilot control and an aircraft, a plurality of flight data linked with the aircraft, wherein a flight datum of the plurality of flight data comprises a flight component datum informing on an operation of a flight component, wherein the flight component comprises a propulsor component;
determining, by the flight controller, a flight boundary for the aircraft as a function of the plurality of flight data;
setting, by the flight controller, an aircraft movement limit as a function of the flight boundary, wherein setting an aircraft movement limit comprises receiving instruction, which includes an aircraft identifier and a specified value of the aircraft movement limit;
receiving, by the flight controller, the thrust envelope, wherein the thrust envelope comprises an instruction to set thrust envelope parameter; and
generating, by the flight controller, a control signal for the aircraft as a function of the aircraft movement limit and the thrust envelope, wherein the control signal limits the aircraft to remain within the flight boundary;
receiving, using an electric propulsor communicatively connected to the flight controller, the control signal; and
controlling operation of the electric propulsor as a function of the control signal.
12. The method of claim 11 , wherein the flight boundary defines a three dimensional space for a flight trajectory of the aircraft.
13. The method of claim 11 , wherein determining the flight boundary for the aircraft further comprises:
training a machine-learning process with training data correlating aircraft flight data and aircraft flight boundary data; and
generating the flight boundary for the aircraft as a function of the machine-learning process.
14. The method of claim 11 , wherein the plurality of flight data comprises a weather datum.
15. The method of claim 11 , wherein the plurality of flight data comprises a location datum.
16. The method of claim 11 , wherein the plurality of flight data comprises a flight component datum.
17. The method of claim 11 , wherein the plurality of flight data comprises an energy capacity datum.
18. The method of claim 11 , wherein the plurality of flight data comprises an aircraft identity datum.
19. The method of claim 11 , wherein the aircraft comprises an electric aircraft.
20. The method of claim 11 , wherein the aircraft comprises an electric vertical takeoff and landing (eVTOL) aircraft.