Autonomous Aircraft Health Systems and Methods
US-2018362190-A1 · Dec 20, 2018 · US
US12424107B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12424107-B2 |
| Application number | US-202217890613-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 18, 2022 |
| Priority date | Aug 25, 2021 |
| Publication date | Sep 23, 2025 |
| Grant date | Sep 23, 2025 |
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A computer-implemented method of enabling optimisation of trajectory for a vehicle, the method comprising: determining a trajectory for the vehicle using: an algorithm; a vehicle model defining path constraints for the vehicle through space; a propulsion system model defining parameters of a propulsion system of the vehicle; an objective function defining one or more objectives; and controlling output of the determined trajectory.
Opening claim text (preview).
We claim: 1. A computer-implemented method of enabling optimisation of trajectory for a vehicle, the computer-implemented method comprising: determining a trajectory for the vehicle and a derate for a propulsion system using: an algorithm; a vehicle model defining path constraints for the vehicle through space; a propulsion system model defining parameters of the propulsion system of the vehicle; and an objective function defining one or more objectives, wherein the algorithm uses the vehicle model, the propulsion system model, and the objective function as inputs to determine the trajectory for the vehicle, the determined trajectory being an optimized trajectory; and wherein the algorithm uses the vehicle model, the propulsion system model, and the objective function as inputs to optimize the derate for the propulsion system; and controlling output of the determined trajectory and the determined derate. 2. The computer-implemented method as claimed in claim 1 , wherein controlling output includes controlling storage of the determined trajectory in a memory. 3. The computer-implemented method as claimed in claim 1 , wherein controlling output includes controlling output of the determined trajectory to an automated vehicle control system. 4. The computer-implemented method as claimed in claim 3 , wherein the automated vehicle control system is an automatic flight control system. 5. The computer-implemented method as claimed in claim 1 , further comprising: determining one or more vehicle operational parameters using the determined trajectory. 6. The computer-implemented method as claimed in claim 5 , further comprising: controlling operation of the vehicle using the determined one or more vehicle operational parameters. 7. The computer-implemented method as claimed in claim 5 , wherein the determined one or more vehicle operational parameters comprises at least one of a vehicle orientation demand and a propulsion system thrust demand. 8. The computer-implemented method as claimed in claim 1 , wherein determining the trajectory of the vehicle further comprises using a navigation model defining navigation constraints for the vehicle. 9. The computer-implemented method as claimed in claim 8 , further comprising: receiving navigation data for a location of the vehicle; and determining the navigation constraints using the received navigation data and the navigation model. 10. The computer-implemented method as claimed in claim 1 , wherein the one or more objectives of the objective function comprises: degradation of the propulsion system; acoustic emissions of the propulsion system; combustion emissions of the propulsion system; and energy consumption of the propulsion system. 11. The computer-implemented method as claimed in claim 1 , wherein the algorithm is an optimisation algorithm. 12. The computer-implemented method as claimed in claim 1 , wherein the parameters of the propulsion system include one or more of: operational parameters of the propulsion system; and health parameters of the propulsion system. 13. The computer-implemented method as claimed in claim 1 , wherein the vehicle is an aircraft and the determined trajectory is for a take-off flight phase and a climb flight phase of the aircraft. 14. A non-transitory computer readable storage medium comprising computer readable instructions that, when executed by a computer, cause performance of the computer-implemented method as claimed in claim 1 . 15. An apparatus for enabling optimisation of trajectory for a vehicle, the apparatus comprising: a controller configured to perform the computer-implemented method as claimed in claim 1 . 16. The apparatus as claimed in claim 15 , wherein the apparatus comprises an electronic flight bag. 17. The apparatus as claimed in claim 15 , wherein the apparatus comprises a flight management system. 18. The apparatus as claimed in claim 15 , wherein the apparatus comprises a data centre, remote from the vehicle.
for a single aircraft · CPC title
for take-off · CPC title
using automatic pilot · CPC title
specially adapted for take-off · CPC title
specially adapted for aircraft · CPC title
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