Method of optimizing a flight plan
A method of optimizing a flight plan of an aircraft used in a flight management system of an aircraft is disclosed. This method makes it possible to constrain the real cost index of the mission executed to the optimal cost index CI opt predetermined by the aircraft operator, by acting on objectives ETA opt and EFOB opt of values of ETA and of EFOB to be achieved. Objectives are linked to this optimal cost index, in order to make the system return from a cost index CI m to the optimal cost index CI opt , while taking account of various constraints imposed by the ATC or the CTFM. Both constraints m ext influence the cost index and constraints which limit the field of possible solutions.
1. A method of optimizing monitoring of a flight plan of an aircraft relative to a predetermined cost index predetermined by an operator, the flight plan including a determined set of waypoints to be overflown by the aircraft, the method implemented by a flight management system and comprising:
computing an optimal flight plan based on the predetermined cost index and computing optimal values of an arrival time and of a quantity of fuel remaining on board that are estimated to destination for the optimal flight plan and the predetermined cost index, the optimal flight plan defining for said determined set of waypoints a longitudinal speed profile and a vertical trajectory;
applying the optimal flight plan as the flight plan to be followed by the aircraft; and
when at least one external constraint causes the flight plan followed by the aircraft to depart from the optimal flight plan, activating a corrective loop for overriding the flight plan to the predetermined cost index, wherein the corrective loop comprises:
computing current values of the arrival time and the quantity of fuel remaining estimated to destination for the flight plan,
detecting two differences including the difference of the current to the optimal values of an arrival time destination and the difference of the current to the optimal values of a quantity of fuel remaining on board at destination,
determining a corrective cost index based on an overriding criteria minimizing each of the two differences,
computing temporary corrections to the longitudinal speed profile and/or the vertical trajectory on at least a portion of the remaining flight plan based on said corrective cost index,
applying the temporary corrections based on said corrective cost index on said at least portion of the remaining flight plan, and then
applying the optimal flight plan based on the predetermined cost index for any remaining flight plan left.
2. The method according to claim 1 , wherein
the optimal flight plan is computed relative to initial flight parameters comprising the optimal cost index, and
corrections to the current flight plan are computed relative to modified flight parameters comprising the corrective cost index and said at least one external constraint.
3. The method according to claim 1 , wherein the overriding criteria uses a strategy based on a modellable cost in the flight management system, and the modellable cost includes at least one of a cost of the time, a cost of the fuel, or a cost of nuisance.
4. The method according to claim 1 , wherein said determining is bound to a field of possible solutions defined by constraints including air traffic control constraints.
5. The method according to claim 4 , wherein the field of possible solutions is defined by constraints including air traffic control and a required time slot at arrival constraints.
6. The method according to claim 1 , wherein the corrective cost index is in a form of an M-uplet of M elementary corrective cost index, M being an integer at least equal to 2, each elementary corrective cost index being applied on an associated flight plan segment, each flight plan segment being a flight plan segment between two waypoints of the determined set of waypoints.
7. The method according to claim 6 , further comprising:
segmenting the optimal flight plan into M segments, the segments being defined over one, several or all of the flight phases of the flight plan, and
associating with each segment j thus defined, j being an integer from 1 to M, of an elementary cost index on this segment, set at the value of the predetermined cost index,
wherein, on detection of one or more external constraints modifying the optimal flight plan, the overriding process supplies as an output a corrective elementary cost index M-uplet, each elementary corrective cost index having to be applied as a new elementary cost index on the associated flight plan segment.
8. The method according to claim 7 , wherein the number M is chosen according to the flight time.
9. The method according to claim 7 , wherein there are as many segments j as branches between waypoints and points characteristic of the flight phases that are segmented.
10. The method according to claim 7 , wherein M is at least equal to 3, defined on a climb phase, a cruise phase and a descent phase of the optimal flight plan, with a first segment 1 corresponding to the climb flight phase, N segments on the cruise flight phase, N being an integer at least equal to 1 and an Mth segment M corresponding to the descent flight phase.
11. The method according to claim 7 , wherein M is equal to 2, the dividing step defining two segments on the cruise phase of the optimal flight plan.
12. A flight management system of an aircraft using a method of optimizing monitoring of a flight plan including a determined set of waypoints to be overflown by the aircraft, with respect to a predetermined cost index, the predetermined cost index predetermined by an operator, the method comprising:
computing an optimal flight plan based on the predetermined cost index and computing optimal values of an arrival time and of a quantity of fuel remaining on board that are estimated to destination for the optimal flight plan and the predetermined cost index, the optimal flight plan defining for said determined set of waypoints a longitudinal speed profile and a vertical trajectory;
applying the optimal flight plan as the flight plan to be followed by the aircraft; and
when at least one external constraint causes the flight plan followed by the aircraft to depart from the optimal flight plan, activating a corrective loop for overriding the flight plan to the predetermined cost index, wherein the corrective loop comprises:
computing current values of the arrival time and the quantity of fuel remaining estimated to destination for the modified flight plan,
detecting two differences including the difference of the current to the optimal values of an arrival time destination and the difference of the current to the optimal values of a quantity of fuel remaining on board at destination,
determining a corrective cost index based on an overriding criteria minimizing each of the two differences,
computing temporary corrections to the longitudinal speed profile and/or the vertical trajectory on at least a portion of the remaining flight plan based on the corrective cost index,
applying temporary corrections based on said corrective cost index on said at least a portion of the remaining flight plan, and then
applying the optimal flight plan based on the predetermined cost index for any remaining flight plane and flight time left.
13. The flight management system according to claim 12 , wherein the corrective cost index is in a form of an M-uplet of M elementary corrective cost index, each elementary corrective cost index being applied on an associated flight plan segment each flight plan segment being a flight plan segment between two waypoints of the determined set of waypoints.
14. The method according to claim 2 , wherein the overriding criteria uses a strategy based on a modellable cost in the flight management system, and the modellable cost includes at least one of a cost of the time, a cost of the fuel, or a cost of nuisance.