Trajectory monitoring
A method for monitoring the flight trajectory of an aircraft comprises the steps reiterated in time consisting in receiving and comparing two trajectory objects, the trajectory objects being associated with two initially identical flight trajectories determined independently of each other over time; and, in case of difference between the two trajectory objects, determining a failed trajectory from the two flight trajectories by comparison with the last known state without fault, the last known state without fault corresponding to two identical trajectory objects. Developments describe the use of flight plan segments, of signatures, fault isolation simultaneously to a change of current leg, the use of levels of operational safety according to an RNP-AR procedure and the notification of the pilot of the trajectory determined as having failed. Software and system aspects are also described.
1. A computer-implemented method for monitoring a flight trajectory of an aircraft comprising the steps reiterated in time of:
receiving and comparing two trajectory objects in at least one Flight Management System, said trajectory objects being associated with two initially identical flight trajectories determined independently of each other over time;
at a given instant, in case of difference between the two trajectory objects in the at least one Flight Management System, determining a failed trajectory from the two flight trajectories by comparison with a last known state without fault, the last known state without fault corresponding to two identical trajectory objects; and
notifying a pilot of the aircraft of a determination of the failed trajectory.
2. The computer-implemented method according to claim 1 , wherein the trajectory objects comprise complete flight trajectories.
3. The computer-implemented method according to claim 1 , wherein the trajectory objects comprise trajectory sections comprising one or more flight plan segments.
4. The computer-implemented method according to claim 3 , wherein the trajectory objects comprise trajectory sections comprising one or more TF (Track to Fix) and/or RF (Radius to Fix) type legs.
5. The computer-implemented method according to claim 1 , wherein the trajectory objects comprise trajectory signatures.
6. The computer-implemented method according to claim 1 , further comprising the steps of:
receiving an indication of a change of a current leg,
comparing in a Flight Warning System the two trajectory objects before and after the change of a current leg.
7. The computer-implemented method according to claim 6 , further comprising determining an existence of a failed trajectory from the two initially identical flight trajectories determined independently of each other over time if the two objects after change of leg are not equal.
8. The computer-implemented method according to claim 6 , further comprising determining the failed trajectory from the two initially identical flight trajectories determined independently of each other over time if the two objects after change of leg are not equal, said determination comprising:
comparing for each of the two trajectory objects, a next trajectory section such as planned before change of current leg and a current trajectory section such as flown after change of current leg; and
determining the failed trajectory as being that associated with the trajectory object for which the next trajectory section such as planned before change of current leg is not equal to the current trajectory section such as flown after change of current leg.
9. The computer-implemented method according to claim 1 , further comprising receiving a level of operational safety and the comparing the trajectory objects being carried out using a fault tolerance threshold, said fault tolerance threshold being predefined depending on the received level of operational safety.
10. The computer-implemented method according to claim 9 , wherein the level of safety being associated with RNP (Required Navigation Performance) values comprised between 0.1 and 1 nautical mile for an RNP-AR (Required Navigation Performance - Authorization Required) type procedure.
11. The computer-implemented method according to claim 1 , wherein the comparing the trajectory objects being carried out at an expiry of a predefined delay.
12. The computer-implemented method according to claim 1 , wherein notifying the pilot further comprises notifying the pilot of the aircraft of the failed trajectory from the two trajectories determined independently of each other over time.
13. A non-transitory computer program product, said non-transitory computer program comprising code instructions for monitoring a flight trajectory of an aircraft when said non-transitory computer program is executed by a computer, the code instructions comprising:
receiving and comparing two trajectory objects in at least one Flight Management System, said trajectory objects being associated with two initially identical flight trajectories determined independently of each other over time;
at a given instant, in case of difference between the two trajectory objects in the at least one Flight Management System, determining a failed trajectory from the two flight trajectories by comparison with a last known state without fault, the last known state without fault corresponding to two identical trajectory objects; and
notifying a pilot of the aircraft of a determination of the failed trajectory.
14. A system for monitoring a flight trajectory of an aircraft, the system comprising two flight management systems or FMSs, and comprising:
the system being configured to receive and compare two trajectory objects in at least one Flight Management System, said trajectory objects being associated with two initially identical flight trajectories determined independently of each other over time;
the system further being configured to, at a given instant, in case of difference between the two trajectory objects in the at least one Flight Management System, determine a failed trajectory from the two flight trajectories by comparison with a last known state without fault, the last known state without fault corresponding to two identical trajectory objects; and
the system further being configured to notify a pilot of the aircraft of a determination of the failed trajectory.
15. The system according to claim 14 , her comprising two Flight Warning Systems configured to monitor the two flight management systems.