Maximum takeoff weight determination for aircraft
An aircraft has a first principles takeoff processor (PCE), a predictive flight envelope protection processor (PFEP), and a maximum takeoff weight processor. The PCE is programmed to predict a liftoff location and an energy state of the aircraft at a liftoff on a runway. The PFEP is programmed to assess each of a plurality of potential trajectories for compliance with or violation of a predetermined flight envelope. The maximum weight processor is programmed to: indicate that the aircraft may takeoff at the aircraft weight when any one of the plurality of potential trajectories is in compliance with the predetermined flight envelope; iteratively reduce an input of the aircraft weight to the PCE until the PCE indicates that any one of the plurality of potential trajectories is in compliance with the predetermined flight envelope; and indicate that the input of the aircraft weight as reduced is a maximum allowable takeoff weight.
1. An aircraft takeoff weight protection system, comprising:
at least one processor configured to:
iteratively selecting input aircraft weights for an aircraft and for each selected input aircraft weight:
predict a liftoff location on a specified runway and an energy state of the aircraft at liftoff from the specified runway based at least in part on the selected input aircraft weight and on environmental conditions;
generate a plurality of potential trajectories of the aircraft from the liftoff location on the specified runway based on the predicted energy state of the aircraft at liftoff from the specified runway;
assess each of the plurality of potential trajectories to determine if any of the plurality of potential trajectories are in compliance with a predetermined flight envelope; and
select as a maximum allowable takeoff weight for the aircraft an input aircraft weight where at least one of the plurality of potential trajectories is assessed to be in compliance with the predetermined flight envelope.
2. The aircraft takeoff weight protection system of claim 1 , wherein the at least one processor is further configured to predict the liftoff location on the specified runway and the energy state of the aircraft at liftoff from the specified runway based further on an engine loss at a decision point past which the aircraft may not be able to stop within a remaining runway length.
3. The aircraft takeoff weight protection system of claim 2 , wherein the at least one processor is configured to generate the plurality of potential trajectories based further on operation of the aircraft with the engine loss.
4. The aircraft takeoff weight protection system of claim 1 , wherein the at least one processor is configured to assess each of the plurality of potential trajectories to determine if any of the plurality of potential trajectories are in compliance with a predetermined flight envelope by determining if any of the plurality of potential trajectories are in compliance with terrain clearance distances.
5. The aircraft takeoff weight protection system of claim 1 , wherein the at least one processor is configured to assess each of the plurality of potential trajectories to determine if any of the plurality of potential trajectories are in compliance with a predetermined flight envelope by determining if any of the plurality of potential trajectories are in compliance with operational limits.
6. The aircraft takeoff weight protection system of claim 1 , wherein the at least one processor is configured to iteratively select input aircraft weights by using a maximum gross weight of the aircraft as an initial value of the selected input aircraft weight and reducing the selected input aircraft weight until at least one of the plurality of potential trajectories is in compliance with the predetermined flight envelope.
7. The aircraft takeoff weight protection system of claim 1 , wherein the at least one processor is further configured to alert a crew responsive to an estimated weight of the aircraft being greater than the maximum allowable takeoff weight.
8. The aircraft takeoff weight protection system of claim 1 , wherein the at least one processor is further configured to determine a maximum amount of fuel that may be carried on the aircraft based on the maximum allowable takeoff weight.
9. The aircraft takeoff weight protection system of claim 1 , wherein the at least one processor is further configured to predict the liftoff location on the specified runway and the energy state of the aircraft at liftoff from the specified runway based further on a weight balance of the aircraft and wind, temperature, and pressure as received from a weather service.
10. The aircraft takeoff weight protection system of claim 1 , wherein the at least on processor is configured to predict the liftoff location on the specified runway and the energy state of the aircraft at liftoff from the specified runway based further on a runway dimension and a starting point for takeoff on the specified runway as received from an airport database.
11. An aircraft takeoff weight protection system, comprising:
at least one processor configured to:
iteratively selecting input aircraft weights for an aircraft and for each selected input aircraft weight:
predict a liftoff location on a specified runway and an energy state of the aircraft at liftoff from the specified runway based at least in part on the selected input aircraft weight and on environmental conditions and on an engine loss at a decision point past which the aircraft may not be able to stop within a remaining runway length, where the environmental conditions include wind, temperature and pressure;
generate a plurality of potential trajectories of the aircraft from the liftoff location on the specified runway based on the predicted energy state of the aircraft at liftoff from the specified runway and based further on operation of the aircraft with the engine loss;
assess each of the plurality of potential trajectories to determine if any of the plurality of potential trajectories are in compliance with a predetermined flight envelope, including terrain clearance distances and operational limits; and
select as a maximum allowable takeoff weight for the aircraft an input aircraft weight where at least one of the plurality of potential trajectories is assessed to be in compliance with the predetermined flight envelope.
12. An aircraft, comprising:
at least one processor configured to:
iteratively selecting input aircraft weights for the aircraft and for each selected input aircraft weight:
predict a liftoff location on a specified runway and an energy state of the aircraft at liftoff from the specified runway based at least in part on the selected input aircraft weight and on environmental conditions;
generate a plurality of potential trajectories of the aircraft from the liftoff location on the specified runway based on the predicted energy state of the aircraft at liftoff from the specified runway;
assess each of the plurality of potential trajectories to determine if any of the plurality of potential trajectories are in compliance with a predetermined flight envelope; and
select as a maximum allowable takeoff weight for the aircraft an input aircraft weight where at least one of the plurality of potential trajectories is assessed to be in compliance with the predetermined flight envelope.
13. The aircraft of claim 12 , wherein the at least one processor is further configured to predict the liftoff location on the specified runway and the energy state of the aircraft at liftoff from the specified runway based further on an engine loss at a decision point past which the aircraft may not be able to stop within a remaining runway length.
14. The aircraft of claim 13 , wherein the at least one processor is configured to generate the plurality of potential trajectories based further on operation of the aircraft with the engine loss.
15. The aircraft of claim 12 , wherein the at least one processor is configured to assess each of the plurality of potential trajectories to determine if any of the plurality of potential trajectories are in compliance with a predetermined flight envelope by determining if any of the plurality of potential trajectories are in compliance with terrain clearance distances.
16. The aircraft of claim 12 , wherein the at least one processor is configured to assess each of the plurality of potential trajectories to determine if any of the plurality of potential trajectories are in compliance with a predetermined flight envelope by determining if any of the plurality of potential trajectories are in compliance with operational limits.
17. The aircraft of claim 12 , wherein the at least one processor is configured to iteratively select input aircraft weights by using a maximum gross weight of the aircraft as an initial value of the selected input aircraft weight and reducing the selected input aircraft weight until at least one of the plurality of potential trajectories is in compliance with the predetermined flight envelope.
18. The aircraft of claim 12 , wherein the at least one processor is further configured to alert a crew responsive to an estimated weight of the aircraft being greater than the maximum allowable takeoff weight.
19. The aircraft of claim 12 , wherein the at least one processor is further configured to determine a maximum amount of fuel that may be carried on the aircraft based on the maximum allowable takeoff weight.
20. The aircraft of claim 12 , wherein the at least on processor is configured to predict the liftoff location on the specified runway and the energy state of the aircraft at liftoff from the specified runway based further on a runway dimension and a starting point for takeoff on the specified runway as received from an airport database.