System and method for operating an aircraft during a climb phase of flight
A system and a method for operating an aircraft during a climb phase of flight include a control unit configured to receive data regarding one or both of a current flight or one or more previous flights of the aircraft from one or more sensors of the aircraft. The control unit is further configured to determine efficient climb phase parameters for the aircraft based on the data. The aircraft is operated during the climb phase of one or both of the current flight or one or more future flights according to the efficient climb phase parameters.
1. A system for operating an aircraft during a climb phase of flight, the system comprising:
a control unit configured to receive data regarding aspects of the aircraft before and during the climb phase of one or both of a current flight or one or more previous flights of the aircraft from one or more sensors of the aircraft,
wherein the control unit is further configured to determine climb phase parameters for the aircraft based on the data regarding the aspects of the aircraft before and during the climb phase of one or both of the current flight or the one or more previous flights of the aircraft, and wherein the aircraft is operated during the climb phase of one or both of the current flight or one or more future flights according to the climb phase parameters.
2. The system of claim 1 , further comprising the one or more sensors.
3. The system of claim 2 , wherein the one or more sensors comprise one or more flight recorders.
4. The system of claim 3 , wherein the one or more sensors further comprise one or more speed sensors, one or more altitude sensors, one or more position sensors, one or more ambient sensors, and one or more weight sensors.
5. The system of claim 1 , wherein the control unit is onboard the aircraft.
6. The system of claim 1 , wherein the control unit is configured to determine the climb phase parameters for a future flight of the aircraft based on the data received from one or more previous flights of the aircraft.
7. The system of claim 1 , wherein the control unit is configured to determine the climb phase attributes by generating one or more climb phase neural network models for the aircraft based on the data.
8. The system of claim 1 , wherein the control unit is further configured to show the climb phase attributes on a monitor within a flight deck of the aircraft.
9. The system of claim 1 , wherein the control unit is configured to determine the climb phase attributes by determining a lowest cost index from a plurality of cost indices.
10. The system of claim 1 , wherein the control unit is further configured to automatically operate controls of the aircraft during the climb phase according to the climb phase parameters.
11. A method for operating an aircraft during a climb phase of flight, the method comprising:
receiving, by a control unit, data regarding aspects of the aircraft before and during the climb phase of one or both of a current flight or one or more previous flights of the aircraft from one or more sensors of the aircraft; and
determining, by the control unit, climb phase parameters for the aircraft based on the data aspects of the aircraft before and during the climb phase of one or both of the current flight or the one or more previous flights of the aircraft, wherein the aircraft is operated during the climb phase of one or both of the current flight or one or more future flights according to the climb phase parameters.
12. The method of claim 11 , wherein the one or more sensors comprise one or more flight recorders.
13. The method of claim 12 , wherein the one or more sensors further comprise one or more speed sensors, one or more altitude sensors, one or more position sensors, one or more ambient sensors, and one or more weight sensors.
14. The method of claim 11 , further comprising disposing the control unit onboard the aircraft.
15. The method of claim 11 , wherein said determining comprises determining the climb phase parameters for a future flight of the aircraft based on the data received from one or more previous flights of the aircraft.
16. The method of claim 11 , wherein said determining comprises determining the climb phase attributes by generating one or more climb phase neural network models for the aircraft based on the data.
17. The method of claim 11 , further comprising showing, by the control unit, the climb phase attributes on a monitor within a flight deck of the aircraft.
18. The method of claim 11 , wherein said determining comprises determining the climb phase attributes by determining a lowest cost index from a plurality of cost indices.
19. The method of claim 11 , further comprising automatically operating, by the control unit, controls of the aircraft during the climb phase according to the climb phase parameters.
20. A non-transitory computer-readable storage medium comprising executable instructions that, in response to execution, cause one or more control units comprising a processor, to perform operations comprising:
receiving data regarding aspects of the aircraft before and during the climb phase of one or both of a current flight or one or more previous flights of an aircraft from one or more sensors of the aircraft; and
determining efficient climb phase parameters for the aircraft based on the data aspects of the aircraft before and during the climb phase of one or both of the current flight or the one or more previous flights of an aircraft, wherein the aircraft is operated during a climb phase of one or both of the current flight or one or more future flights according to the efficient climb phase parameters.