Patent ID: 11922660
Assignee: AIRBUS SAS
Field: Computer technology (Electrical engineering)
Classification: CPC G  B | IPC B  G

Claim 1:
2. The method according to claim 1, in which the adjustment step comprises:
in absence of a preceding iteration, the substeps of comparison of pixels of the profile with pixels of the outline of the leading aircraft and of identification of control points of the outline of the leading aircraft which correspond, respectively, to control points of the profile to obtain pairs of control points;
in presence of a preceding iteration, the substeps of determination of a new profile of the leading aircraft from the three-dimensional model of the leading aircraft as a function of data from the preceding iteration, of comparison of the pixels of the new profile with the pixels of the outline of the leading aircraft and of identification of the control points of the outline of the leading aircraft which correspond, respectively, to control points of the new profile, to obtain pairs of control points;
in all cases, a substep of calculation of a distance between the control points of each pair of control points and of the value of the score of the iteration corresponding to a sum of the distances determined for the set of pairs.