Patent ID: 11884379
Assignee: DASSAULT AVIATION
Field: Mechanical elements (Mechanical engineering)
Classification: CPC B  G | IPC B  G

Claim 6:
7. The control system according to claim 6, wherein the control unit is configured to determine whether the high lift assembly has finished switching to the commanded aerodynamic configuration, and each marker is further configured to switch into a transitional on configuration,
the visual indication device being configured to control, after receiving a signal representative of the generated control vector, a transition of the associated marker from the off configuration to the transitional on configuration;
the visual indication device being configured to command, after the high-lift assembly has finished switching to the commanded aerodynamic configuration, the switching of the associated marker from the transitional on configuration to the illuminated on configuration;
wherein the transitional on configuration is a flashing configuration of each marker, and/or each marker is configured to emit a light intensity having a first predetermined color in the illuminated on configuration and having a second predetermined color distinct from the first color in the transitional on configuration.