The present invention relates to a method for computing a setpoint trajectory of an aircraft comprising at least two subsets. It is characterized in that it comprises the formulation and the solving of an optimization problem for the trajectory, and that the formulation of the said problem comprises at least the formulation of a constraint related to a transition of legs on at least one first subset of the trajectory, and the formulation of a constraint related to a transition of vertical flight phases on at least one second subset of the trajectory. The invention also relates to a system and a computer program for the computation of a trajectory.
METHOD OF COMPUTING AIRCRAFT TRAJECTORY SUBJECT TO LATERAL AND VERTICAL CONSTRAINTS
2016-06-09
Patent
Elektronische Ressource
Englisch
IPC: | G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS |
Method of computing aircraft trajectory subject to lateral and vertical constraints
Europäisches Patentamt | 2018
|System and method for optimizing aircraft lateral and vertical trajectory for published procedures
Europäisches Patentamt | 2017
|Vertical and Lateral Trajectory Coupling Method in 4D Trajectory Prediction
Springer Verlag | 2023
|