Method and system for resetting a digital model

1. A method of resetting a basic digital model, the method comprising:

detecting a stable state of a first parameter of said basic digital model, the first parameter being representative of a signal delivered by a sensor, the basic digital model representing a relationship between the first parameter and a second parameter;

during said stable state of said first parameter, obtaining a resetting parameter for said basic digital model as a function of said first parameter, of the second parameter of said basic digital model, and of said basic digital model;

obtaining a reset model of the basic digital model based on the basic digital model and the resetting parameter; and

regulating a turbojet using the reset model, wherein

said basic digital model is a gain relationship giving a ratio between two temperatures at two different stages of the turbojet as a function of a speed of rotation of a fan of said turbojet,

said first parameter is one of said temperatures, and

said second parameter is said speed of rotation.

2. The method according to claim 1 , further comprising:

subdividing the domain of possible values for said second parameter into a plurality of ranges;

determining and storing the range in which the second parameter is to be found during the stable state of the first parameter; and

calculating or estimating a local resetting value and allocating said local resetting value to at least one of said ranges,

wherein said resetting parameter is obtained from local resetting values allocated to at least one of said ranges and a current value of said second parameter.

3. The method according to claim 2 , wherein said local resetting value allocated to one of said ranges is a value allocated to another one of said ranges, said other range being determined on the basis of a truth table.

4. The method according to claim 2 , further comprising, for at least one portion of said domain of possible values, interpolating said resetting parameter from at least one of said local resetting values.

5. The method according to claim 2 , further comprising:

implementing said method in said turbojet once and once only per flight; and

after determining the range in which the second parameter is to be found, storing in a non-volatile memory associated with said range, both said second parameter and said local resetting value.

6. The method according to claim 1 , further comprising calculating a corrected value for said first parameter on the basis of a current value of the first parameter and of the reset model.

7. The method according to claim 5 , wherein said storing of the range in which the second parameter is to be found is performed on condition of a positive result from verifying that an engine of a turbojet is in the started state.

8. The method according to claim 5 , further comprising smoothing the resetting parameter.

9. A system for resetting a basic digital model, the system comprising:

a detection circuit configured to detect a stable state of a first parameter of said basic digital model, the first parameter being representative of a signal delivered by a sensor, the basic digital model representing a relationship between the first parameter and a second parameter;

a circuit configured, during said stable state of said first parameter, to obtain a resetting parameter for said basic digital model as a function of said first parameter, of the second parameter of said basic digital model, and of said basic digital model;

a circuit configured to obtain a reset model of the basic digital model based on said basic digital model and from the resetting parameter; and

a circuit configured to use the reset model, instead of the first parameter of the basic digital model, to regulate a turbojet, wherein

said basic digital model is a gain relationship giving a ratio between two temperatures at two different stages of the turbojet as a function of a speed of rotation of a fan of said turbojet,

said first parameter is one of said temperatures, and

said second parameter is said speed of rotation.

10. The turbojet, comprising the system according to claim 9 for resetting the basic digital model.

11. The method according to claim 5 , further comprising, in order to regulate said turbojet, using said first parameter of the reset model, instead of the first parameter representative of the signal delivered by the sensor, the signal delivered by said sensor being used only for resetting said basic digital model and for obtaining said reset model.