METHOD OF COMPUTING AIRCRAFT TRAJECTORY SUBJECT TO LATERAL AND VERTICAL CONSTRAINTS

摘要

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.

主权项

1. A method for computing a setpoint trajectory of an aircraft, the trajectory defining at least successive values of lateral position, altitude, and speed of the aircraft, the trajectory comprising at least two subsets, the method comprising at least:
a step of formulating at least one optimization problem for the trajectory for at least one optimization criterion, the formulating step comprising at least:
a sub-step of formulating at least one constraint related to a transition of legs on at least one first subset of the trajectory;a sub-step of formulating at least one constraint related to a transition of vertical flight phases on at least one second subset of the trajectory;a step of solving the optimization problem for the trajectory.