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

Claim 8:
9. The control system according to claim 2, wherein the high-lift assembly is configured to be controlled to switch from a current one of the aerodynamic configurations to at least one other possible aerodynamic configuration of the aerodynamic configurations,
the control system further comprising a sensor system for flight parameters of the aircraft, the lift control unit being connected to sensors of the sensor system, the lift control unit being configured to determine, for each possible aerodynamic configuration, an authorization or prohibition of switching to the possible aerodynamic configuration as a function of signals received from the sensors of the sensor system;
the manual control device comprising a visual indication device configured to display, to a pilot of the aircraft and for each possible aerodynamic configuration, at least one light representative of the determined authorization or prohibition of switching to the possible aerodynamic configuration.